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Aeronautical Research Committee, reports and memoranda

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Aeronautical Research Committee, reports and memoranda

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Great Britain. Aeronautical Research Committee
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Related materials as well as pre- and post-revision versions

The lateral stability of S.E.5a in gliding flightLeave the NDL website. Report on the influence of calcium and of calcium plus silicon on aluminiumLeave the NDL website. The no. 2 7-foot wind channel at the royal aircraft establishmentLeave the NDL website. Determination of lift and drag coefficients during a stall by means of accelerometersLeave the NDL website. R.A.E. electrical indicator for high speed internal combustion engines, also pressure gauge for maximum pressuresLeave the NDL website. The effect of shear upon a framework of uniform rectangular cross-sectionLeave the NDL website. The force on an aileron balanced byntheb "Backward Hinge" methodsLeave the NDL website. The prevention of fire in single-engined aeroplanes : report of the Fire Prevention Sub-committeeLeave the NDL website. Lift and drag of B.E.2E with R.A.F.19 wings. Comparison of full scale and model resultsLeave the NDL website. Scale effect on struts and drag of wiring plates of a bristol fighter, correction of model tests for comparison with the full scaleLeave the NDL website. Tests on improved models of aircraft compassesLeave the NDL website. Tests on a model of the dreadnought postal type monoplaneLeave the NDL website. The effect of a large boss on airscrew performanceLeave the NDL website. Fire experiments with various types of fireproof bulkheadsLeave the NDL website. Experiments on rigid airship R.29.Leave the NDL website. Some experiments on airscrews at zero torque with applications to a helicopter descending with engine "off," and to the design of windmillsLeave the NDL website. Model tests of 64 section biplane wings with flapsLeave the NDL website. The equilibrium of R.38 in circling flightLeave the NDL website. The resistance of a spheroid, with special reference to the effect of wires placed around the model in a plane at right angles to the axisLeave the NDL website. Interference on characteristics of aerofoil in wind tunnel of rectangular sectionLeave the NDL website. The comparison of the manœuvrability of aeroplanes by the use of a cinematograph cameraLeave the NDL website. A direction and velocity meter for use in wind tunnel workLeave the NDL website. Graphical solutions for inviscid flowLeave the NDL website. The stability of airshipsLeave the NDL website. Experimental determination of tailplane characteristicsLeave the NDL website. Experiments on airscrews with tractor and pusher bodiesLeave the NDL website. Experiments on rigid airship R.32, Pt.1: Pressures on the upper fin and rudderLeave the NDL website. Air consumption and B.H.P. of aero enginesLeave the NDL website. The rolling and yawing moments of an aerofoil in straight flightLeave the NDL website. A continuous rotation balance for the measurement of L, at small rates of rollLeave the NDL website. Theoretical stream-lines round a joukowsky aerofoilLeave the NDL website. Lateral control at large angles of incidence. Yawing and rolling moments due to aileron movement on a complete model of S.E.5A.Leave the NDL website. An experimental test of the prandtl correction for tunnel wall interferenceLeave the NDL website. Rolling and yawing moments due to roll of model avro wings, with standard and interplane ailerons, and rudder moments for standard and special large rudderLeave the NDL website. On the aerodynamic characteristics of parachutes : a comprehensive account of researches incorporated in various papers submitted to the Advisory Committee for AeronauticsLeave the NDL website. Measurments of normal force and pitching moment on rigid airship R.33Leave the NDL website. Some aspects of the mutual interference between parts of aircraftLeave the NDL website. Reports and memoranda of the Aeronautical Research Committee published between 1st October 1921 and 31st March 1923Leave the NDL website. Wind tunnel interference on aerofoilsLeave the NDL website. The effect of the airscrew slipstreamLeave the NDL website. The steady adiabatic flow of a gasLeave the NDL website. Phase setting of engine indicatorsLeave the NDL website. Experiments on a model of rigid airship R.32, together with a comparison with the results of full scale turning trials and a consideration of the stability of the shipLeave the NDL website. The aerodynamic loading of airshipsLeave the NDL website. Tail loads in recovering from a vertical dive at terminal velocityLeave the NDL website. Determination of viscosity of cellulose. Cuprammonium hydroxide solutionLeave the NDL website. The manœuvres of inverted flightLeave the NDL website. An electric motor of small diameter for use inside aeroplane modelsLeave the NDL website. Pitot-static tube factor at low reynolds numbersLeave the NDL website. Some suggestions for improving aeroplane control at low speedsLeave the NDL website. The effects of tip speed on airscrew performance : an experimental investigation of the performance of an airscrew over a range of speeds of revolution from "model" speeds up to tip speeds in excess of the velocity of sound in airLeave the NDL website. The production and heat-treatment of chill-castings in an aluminium alloy ("Y")Leave the NDL website. Load factors for commercial heavier-than-air craft : report of the Load Factor Sub-committeeLeave the NDL website. Determination of rotary derivativesLeave the NDL website. Report on the accident to H.M. airship R.38Leave the NDL website. A comparison between the aerodynamic properties of two aerofolis of the same section, but with square and rounded wing tise rounded wing tips respectivelyLeave the NDL website. Tests of R.A.E. gear wheel type petrol pumpLeave the NDL website. Notes on the vortex theory of airscrewsLeave the NDL website. Experiments with a modified thrustmeterLeave the NDL website. Preliminary report on the forced oscillations of aircraft compassesLeave the NDL website. An investigation of the influence of down-wash on the rotary derivative Mq*Leave the NDL website. On the theory of tapered aerofoilsLeave the NDL website. The efficiency of a tandem system of airscrewsLeave the NDL website. Experimental tests of the vortex theory of aerofoilsLeave the NDL website. The reduction of the effective value of young's modulus in flexible compression membersLeave the NDL website. Experiments with a close tandem airscrew pairLeave the NDL website. Description of lift, vertical-force and drag balances for the roof of the duplex wind tunnelLeave the NDL website. The design of tapered wingsLeave the NDL website. A directional hot-wire anemometerLeave the NDL website. Report on the effects of over-heating and repeated melting on aluminiumLeave the NDL website. The calculation of stresses in a redundant structure by the method of comparison of deflections, with examples of its application to aeroplane designLeave the NDL website. Report of the airship stressing panelLeave the NDL website. A simple method for calculating the span and chordwise loading on straight and swept wings of any given aspect ratio at subsonic speedsLeave the NDL website. The prediction of the resistance of rigid airshipLeave the NDL website. The two-dimensional flow of air around an aerofoil of symmetrical sectionLeave the NDL website. The Northerly turning error of compasses in aircraftLeave the NDL website. Methods for calculating the lift distribution of wings : subsonic lifting-surface theoryLeave the NDL website. Experiments on transmission of air waves through pipesLeave the NDL website. Some experiments on the fatigue of materials under alternating torsionLeave the NDL website. Note on measurements of airscrew thrustLeave the NDL website. The constitution and age-hardening of alloys of aluminium with copper, magnesium, and silicon in the solid stateLeave the NDL website. On the use of a slotted trailing flap on aerofoils of various cambersLeave the NDL website. The flutter of aeroplane wingsLeave the NDL website. Seaplanes. Taking off and alightingLeave the NDL website. On castingliano's theorem of least work, and the principle of St. VenantLeave the NDL website. The effect of rate of loading on the apparent strength of cotton balloon fabricLeave the NDL website. The acoustics of moving sources with application to airscrewsLeave the NDL website. Lateral control of bristol fighter at low speedsLeave the NDL website. An aerodynamic theory of the airscrewLeave the NDL website. Lateral control at low speedsLeave the NDL website. The accuracy of the Vortex Theory of Airscrews in the light of recent experimental work and its application to airscrew designLeave the NDL website. On a method for the direct design of framed structures having redundant bracingLeave the NDL website. On the rate of transmission of heat from the walis of an airship passenger carLeave the NDL website. The efficiency of an airscrewLeave the NDL website. The possible causes of fire in an aeroplane crash and the means that can be taken to lessen the fire risk : report of the Fire Prevention Sub-committeeLeave the NDL website. A consideration of airscrew theory in the light of data derived from an experimental investigation of the distribution 0f pressure over the entire surface of an airscrew blade, and also over aerofolis of appropriate shapesLeave the NDL website. The heat-treatment and mechanical properties of alloys of aluminium with small percentages of copperLeave the NDL website. Some applications of the vortex theory of aerofoilsLeave the NDL website. Eddy systems behind discsLeave the NDL website. Vibrations of rafwires . Presented by the Director of Research.Leave the NDL website. An empirical method of predicting the aerodynamic properties of an aerofoilLeave the NDL website. Full scale and model measurements of lift and drag of bristol fighter with R.A.F. 31 wingsLeave the NDL website. The effect of scratches and of various workshop finishes upon the fatigue strength of steelLeave the NDL website. Induced flow through a partially choked pipeLeave the NDL website. On a new means of ascertaining the mean pressurein in a heat engineLeave the NDL website. A memorandum giving a summary of present knowledge on the relation between ground contours, atmospheric turbulence, wind speed and directionLeave the NDL website. The flutter of monoplanes biplanes and tail units : (A sequel to R.& M.1155)Leave the NDL website. Aerodynamic pressure on an airship hull in curviliear flightLeave the NDL website. The effect of a temperature of 212°F. on steel submitted to alternating torsionLeave the NDL website. Wind tunnel for measuring three forces and three momentsLeave the NDL website. On the free transverse vibrations of air-acrew bladesLeave the NDL website. Full scale determination of the characteristics of a variable pitch airscrewLeave the NDL website. Lift and drag of the bristol fighter with wings of three aspect ratiosLeave the NDL website. Eexperiments with model flying boat hulls and seaplane floats : twenty-second series report. comparison of the vigilant straight frame type and curved section flying boatsLeave the NDL website. The Effect of axial loading, torsion, flexure and shear upon a braced tube of any uniform cross sectionLeave the NDL website. The "duplex" wind tunnel of the National Physical LaboratoryLeave the NDL website. Calculation of the rotary derivatives due to yawing for a monoplane wingLeave the NDL website. An investigation of downwash in the slipstreamLeave the NDL website. A graphical method for the determination of the bending moments and deflection in an aerpplane sparLeave the NDL website. Acceleration of aeroplanes in vertical air currentsLeave the NDL website. Pressure distribution over the wings of, and force measurements on, a model B.E.2C biplane with raked wing tipsLeave the NDL website. Tandem aerofoilsLeave the NDL website. The singing of circular and streamline wiresLeave the NDL website. The constitution of some alloys of aluminium with copper and nickelLeave the NDL website. The drag curve of R.A.F. 14 B.E.2E wings.obtained by full scale experiments with airscrew running and with airscrew stationaryLeave the NDL website. The accuracy of sextant observations taken from aircraftLeave the NDL website. Experiments on rigid airship R.38(Z.R. 2)Leave the NDL website. Collected reports on British high speed aircraft for the 1931 Schneider trophy contestLeave the NDL website. Notes on French and Italian aeronautical practice with particular regard to airshipsLeave the NDL website. The motion of airships under certain imposed movements of the ruddersLeave the NDL website. Test on a large aerofoil of R.A.E. 15 sectionLeave the NDL website. Experiments with the family of airscrews mounted in front of a small bodyLeave the NDL website. Full scale and model measurements of pressure distribution round two rib of a B.E.2E aeroplane with R.A.F. 19 sectionLeave the NDL website. The equilibrium of airships in curvilinerar flight : an addendum to R. & M. 716Leave the NDL website. The lift and drag of a standard bristol fighter aeroplaneLeave the NDL website. Wind tunnel interference on wings, bodies and airscrewsLeave the NDL website. Preliminary report on the properties of commercially pure nickel as a standard material for fatique investigationsLeave the NDL website. Physical properties of dope solvent mixtures(continuation of R.& M. 663)Leave the NDL website. Elimination of the static pressure gradient along wind tunnels of the N.P.L. typeLeave the NDL website. The relationship between the number of secondary turns on a magneto armature, and the secondary voltage with shunt resistance. Measurements on a rotating armature magneto : (R.A.E. report E.1979)Leave the NDL website. Flight tests with R.A.E. electrical indicatorLeave the NDL website. Pressure plotting on fin and rudder of a model of R.32Leave the NDL website. Stresses in a stiff jointed polygonal frame under a system of parallel loadsLeave the NDL website. The canonical forms of the equations of motion of an aeroplane in still and gusty airLeave the NDL website. Tests of four slotted aerofoils, supplied by Messrs. Handley Page, Ltd.Leave the NDL website. The interference of wind channel walls on the aerodynamic characteristics of an aerofoilLeave the NDL website. The pressure distribution over a model of the hull of airship R.33Leave the NDL website. The constitution and age-hardening of the ternary alloys of aluminium with magnesium and copperLeave the NDL website. On the effect of placing an airscrew in various positions within the nose of a streamline bodyLeave the NDL website. Experiments on rigid airship R.32, Pt. III : Mesurements on resistance and airspeedLeave the NDL website. Lift and drag of B.E. 2E. with R.A.F. 14 wings. Comparison of full scale and model resoultLeave the NDL website. Some experiments on a model biplane having slotted wings with particular reference to the improvement of lateral control at low speedsLeave the NDL website. Experiments on a model of a rigid airship of new designLeave the NDL website. Some calculations dealing with the disturbed motion of an aeroplane, with special reference to landingLeave the NDL website. Biplane investigation with R.A.F. 15 sectionLeave the NDL website. Collected reports on British high speed aircraft for the 1927 Schneider trophy contestLeave the NDL website. A method of calculating the characteristics of a tapered wingLeave the NDL website. The mechanics of the wöhler rotating bar fatigue testLeave the NDL website. High speed induced wind tunnelLeave the NDL website. Full scale and model measurements of pressure distribution round one rib of a B.E. 2C aeroplane with R.A.F. 15 sectionLeave the NDL website. Lift, drag and pitching moment of the 1/5th scale bristol fighter model in the duplex wind tunnelLeave the NDL website. Corrosion fatigue test on aluminium crystalLeave the NDL website. The Effects of axial loading, flexure, torsion and shear upon a tubular framework with taperLeave the NDL website. The full scale determination of the lateral resistance derivatives of a bristol fighter aeroplaneLeave the NDL website. Comparison of longitudinal with transverse stepsLeave the NDL website. A comparison of the rates of heat dissipation of an underslung and nose radiator on S.E.5(S.E.5a and S.E.5b)Leave the NDL website. The measurement of aeroplane speed with special reference to the use of a suspended static headLeave the NDL website. Wind tunnel tests on a fokker biplane/ By W.L. CowleyLeave the NDL website. The handley page slotted wingLeave the NDL website. Report on further investigations of the effect of sunlight on aeroplane fabricLeave the NDL website. Experiments on rigid airship R.32, Pt. II : Controllability and turning trialsLeave the NDL website. Theoretical relationships for a biplaneLeave the NDL website. The calculation of the characteristics of tapered wingsLeave the NDL website. Fluid motion (theory)Leave the NDL website. Further experiments on tandem aerofoilsLeave the NDL website. On the effect of sideslip on the aerodynamic forces and moments (including those due to the controls) for a model S.E.5a aeroplaneLeave the NDL website. Test of ten aerofoil sections for metal airscrewsLeave the NDL website. The " Rotational Inflow Factor" in propeller theoeyLeave the NDL website. The effect of yaw on the balance of ailerons of the "horn" typeLeave the NDL website. Tests at various staggers and gap chord ratiosLeave the NDL website. Biplane investigation with R.A.F. 15 sectionLeave the NDL website. Report on the viscosity of acetyl cellulose solutionsLeave the NDL website.

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図書
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Alternative Title
ARC R & M
Place of Publication (Country Code)
uk
Text Language Code
en
Target Audience
一般
Related Material
The lateral stability of S.E.5a in gliding flight
Report on the influence of calcium and of calcium plus silicon on aluminium
The no. 2 7-foot wind channel at the royal aircraft establishment
Determination of lift and drag coefficients during a stall by means of accelerometers
R.A.E. electrical indicator for high speed internal combustion engines, also pressure gauge for maximum pressures
The effect of shear upon a framework of uniform rectangular cross-section
The force on an aileron balanced byntheb "Backward Hinge" methods
The prevention of fire in single-engined aeroplanes : report of the Fire Prevention Sub-committee
Lift and drag of B.E.2E with R.A.F.19 wings. Comparison of full scale and model results
Scale effect on struts and drag of wiring plates of a bristol fighter, correction of model tests for comparison with the full scale
Tests on improved models of aircraft compasses
Tests on a model of the dreadnought postal type monoplane
The effect of a large boss on airscrew performance
Fire experiments with various types of fireproof bulkheads
Experiments on rigid airship R.29.
Some experiments on airscrews at zero torque with applications to a helicopter descending with engine "off," and to the design of windmills
Model tests of 64 section biplane wings with flaps
The equilibrium of R.38 in circling flight
The resistance of a spheroid, with special reference to the effect of wires placed around the model in a plane at right angles to the axis
Interference on characteristics of aerofoil in wind tunnel of rectangular section
The comparison of the manœuvrability of aeroplanes by the use of a cinematograph camera
A direction and velocity meter for use in wind tunnel work
Graphical solutions for inviscid flow
The stability of airships
Experimental determination of tailplane characteristics
Experiments on airscrews with tractor and pusher bodies
Experiments on rigid airship R.32, Pt.1: Pressures on the upper fin and rudder
Air consumption and B.H.P. of aero engines
The rolling and yawing moments of an aerofoil in straight flight
A continuous rotation balance for the measurement of L, at small rates of roll
Theoretical stream-lines round a joukowsky aerofoil
Lateral control at large angles of incidence. Yawing and rolling moments due to aileron movement on a complete model of S.E.5A.
An experimental test of the prandtl correction for tunnel wall interference
Rolling and yawing moments due to roll of model avro wings, with standard and interplane ailerons, and rudder moments for standard and special large rudder
On the aerodynamic characteristics of parachutes : a comprehensive account of researches incorporated in various papers submitted to the Advisory Committee for Aeronautics
Measurments of normal force and pitching moment on rigid airship R.33
Some aspects of the mutual interference between parts of aircraft
Reports and memoranda of the Aeronautical Research Committee published between 1st October 1921 and 31st March 1923
Wind tunnel interference on aerofoils
The effect of the airscrew slipstream
The steady adiabatic flow of a gas
Phase setting of engine indicators
Experiments on a model of rigid airship R.32, together with a comparison with the results of full scale turning trials and a consideration of the stability of the ship
The aerodynamic loading of airships
Tail loads in recovering from a vertical dive at terminal velocity
Determination of viscosity of cellulose. Cuprammonium hydroxide solution
The manœuvres of inverted flight
An electric motor of small diameter for use inside aeroplane models
Pitot-static tube factor at low reynolds numbers
Some suggestions for improving aeroplane control at low speeds
The effects of tip speed on airscrew performance : an experimental investigation of the performance of an airscrew over a range of speeds of revolution from "model" speeds up to tip speeds in excess of the velocity of sound in air
The production and heat-treatment of chill-castings in an aluminium alloy ("Y")
Load factors for commercial heavier-than-air craft : report of the Load Factor Sub-committee
Determination of rotary derivatives
Report on the accident to H.M. airship R.38
A comparison between the aerodynamic properties of two aerofolis of the same section, but with square and rounded wing tise rounded wing tips respectively
Tests of R.A.E. gear wheel type petrol pump
Notes on the vortex theory of airscrews
Experiments with a modified thrustmeter
Preliminary report on the forced oscillations of aircraft compasses
An investigation of the influence of down-wash on the rotary derivative Mq*
On the theory of tapered aerofoils
The efficiency of a tandem system of airscrews
Experimental tests of the vortex theory of aerofoils
The reduction of the effective value of young's modulus in flexible compression members
Experiments with a close tandem airscrew pair
Description of lift, vertical-force and drag balances for the roof of the duplex wind tunnel
The design of tapered wings
A directional hot-wire anemometer
Report on the effects of over-heating and repeated melting on aluminium
The calculation of stresses in a redundant structure by the method of comparison of deflections, with examples of its application to aeroplane design
Report of the airship stressing panel
A simple method for calculating the span and chordwise loading on straight and swept wings of any given aspect ratio at subsonic speeds
The prediction of the resistance of rigid airship
The two-dimensional flow of air around an aerofoil of symmetrical section
The Northerly turning error of compasses in aircraft
Methods for calculating the lift distribution of wings : subsonic lifting-surface theory
Experiments on transmission of air waves through pipes
Some experiments on the fatigue of materials under alternating torsion
Note on measurements of airscrew thrust
The constitution and age-hardening of alloys of aluminium with copper, magnesium, and silicon in the solid state
On the use of a slotted trailing flap on aerofoils of various cambers
The flutter of aeroplane wings
Seaplanes. Taking off and alighting
On castingliano's theorem of least work, and the principle of St. Venant
The effect of rate of loading on the apparent strength of cotton balloon fabric
The acoustics of moving sources with application to airscrews
Lateral control of bristol fighter at low speeds
An aerodynamic theory of the airscrew
Lateral control at low speeds
The accuracy of the Vortex Theory of Airscrews in the light of recent experimental work and its application to airscrew design
On a method for the direct design of framed structures having redundant bracing
On the rate of transmission of heat from the walis of an airship passenger car
The efficiency of an airscrew
The possible causes of fire in an aeroplane crash and the means that can be taken to lessen the fire risk : report of the Fire Prevention Sub-committee
A consideration of airscrew theory in the light of data derived from an experimental investigation of the distribution 0f pressure over the entire surface of an airscrew blade, and also over aerofolis of appropriate shapes
The heat-treatment and mechanical properties of alloys of aluminium with small percentages of copper
Some applications of the vortex theory of aerofoils
Eddy systems behind discs
Vibrations of rafwires . Presented by the Director of Research.
An empirical method of predicting the aerodynamic properties of an aerofoil
Full scale and model measurements of lift and drag of bristol fighter with R.A.F. 31 wings
The effect of scratches and of various workshop finishes upon the fatigue strength of steel
Induced flow through a partially choked pipe
On a new means of ascertaining the mean pressurein in a heat engine
A memorandum giving a summary of present knowledge on the relation between ground contours, atmospheric turbulence, wind speed and direction
The flutter of monoplanes biplanes and tail units : (A sequel to R.& M.1155)
Aerodynamic pressure on an airship hull in curviliear flight
The effect of a temperature of 212°F. on steel submitted to alternating torsion
Wind tunnel for measuring three forces and three moments
On the free transverse vibrations of air-acrew blades
Full scale determination of the characteristics of a variable pitch airscrew
Lift and drag of the bristol fighter with wings of three aspect ratios
Eexperiments with model flying boat hulls and seaplane floats : twenty-second series report. comparison of the vigilant straight frame type and curved section flying boats
The Effect of axial loading, torsion, flexure and shear upon a braced tube of any uniform cross section
The "duplex" wind tunnel of the National Physical Laboratory
Calculation of the rotary derivatives due to yawing for a monoplane wing
An investigation of downwash in the slipstream
A graphical method for the determination of the bending moments and deflection in an aerpplane spar
Acceleration of aeroplanes in vertical air currents
Pressure distribution over the wings of, and force measurements on, a model B.E.2C biplane with raked wing tips
Tandem aerofoils
The singing of circular and streamline wires
The constitution of some alloys of aluminium with copper and nickel
The drag curve of R.A.F. 14 B.E.2E wings.obtained by full scale experiments with airscrew running and with airscrew stationary
The accuracy of sextant observations taken from aircraft
Experiments on rigid airship R.38(Z.R. 2)
Collected reports on British high speed aircraft for the 1931 Schneider trophy contest
Notes on French and Italian aeronautical practice with particular regard to airships
The motion of airships under certain imposed movements of the rudders
Test on a large aerofoil of R.A.E. 15 section
Experiments with the family of airscrews mounted in front of a small body
Full scale and model measurements of pressure distribution round two rib of a B.E.2E aeroplane with R.A.F. 19 section
The equilibrium of airships in curvilinerar flight : an addendum to R. & M. 716
The lift and drag of a standard bristol fighter aeroplane
Wind tunnel interference on wings, bodies and airscrews
Preliminary report on the properties of commercially pure nickel as a standard material for fatique investigations
Physical properties of dope solvent mixtures(continuation of R.& M. 663)
Elimination of the static pressure gradient along wind tunnels of the N.P.L. type
The relationship between the number of secondary turns on a magneto armature, and the secondary voltage with shunt resistance. Measurements on a rotating armature magneto : (R.A.E. report E.1979)
Flight tests with R.A.E. electrical indicator
Pressure plotting on fin and rudder of a model of R.32
Stresses in a stiff jointed polygonal frame under a system of parallel loads
The canonical forms of the equations of motion of an aeroplane in still and gusty air
Tests of four slotted aerofoils, supplied by Messrs. Handley Page, Ltd.
The interference of wind channel walls on the aerodynamic characteristics of an aerofoil
The pressure distribution over a model of the hull of airship R.33
The constitution and age-hardening of the ternary alloys of aluminium with magnesium and copper
On the effect of placing an airscrew in various positions within the nose of a streamline body
Experiments on rigid airship R.32, Pt. III : Mesurements on resistance and airspeed
Lift and drag of B.E. 2E. with R.A.F. 14 wings. Comparison of full scale and model resoult
Some experiments on a model biplane having slotted wings with particular reference to the improvement of lateral control at low speeds
Experiments on a model of a rigid airship of new design
Some calculations dealing with the disturbed motion of an aeroplane, with special reference to landing
Biplane investigation with R.A.F. 15 section
Collected reports on British high speed aircraft for the 1927 Schneider trophy contest
A method of calculating the characteristics of a tapered wing
The mechanics of the wöhler rotating bar fatigue test
High speed induced wind tunnel
Full scale and model measurements of pressure distribution round one rib of a B.E. 2C aeroplane with R.A.F. 15 section
Lift, drag and pitching moment of the 1/5th scale bristol fighter model in the duplex wind tunnel
Corrosion fatigue test on aluminium crystal
The Effects of axial loading, flexure, torsion and shear upon a tubular framework with taper
The full scale determination of the lateral resistance derivatives of a bristol fighter aeroplane
Comparison of longitudinal with transverse steps
A comparison of the rates of heat dissipation of an underslung and nose radiator on S.E.5(S.E.5a and S.E.5b)
The measurement of aeroplane speed with special reference to the use of a suspended static head
Wind tunnel tests on a fokker biplane/ By W.L. Cowley
The handley page slotted wing
Report on further investigations of the effect of sunlight on aeroplane fabric
Experiments on rigid airship R.32, Pt. II : Controllability and turning trials
Theoretical relationships for a biplane
The calculation of the characteristics of tapered wings
Fluid motion (theory)
Further experiments on tandem aerofoils
On the effect of sideslip on the aerodynamic forces and moments (including those due to the controls) for a model S.E.5a aeroplane
Test of ten aerofoil sections for metal airscrews
The " Rotational Inflow Factor" in propeller theoey
The effect of yaw on the balance of ailerons of the "horn" type
Tests at various staggers and gap chord ratios
Biplane investigation with R.A.F. 15 section
Report on the viscosity of acetyl cellulose solutions