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An experimental and computational investigation of oscillating airfoil unsteady aerodynamics at large mean incidence [microform] / Vincent R. Capece, Max F. Platzer (NASA/CR-2003-212199)

An experimental and computational investigation of oscillating airfoil unsteady aerodynamics at large mean incidence [microform] / Vincent R. Capece, Max F. Platzer (NASA/CR-2003-212199)
マイクロ図書
2003<YCA-NAS 1.26:212199>
国立国会図書館
  • 件名Unsteady aerodynamics Turbomachinery Airfoils Aeroe...

Unsteady cascade aerodynamic response using a multiphysics simulation code [microform] / C. Lawrence, E. Spyropoulos, T.S.R. Reddy (NASA/TM ; 2000-209635)

Unsteady cascade aerodynamic response using a multiphysics simulation code [microform] / C. Lawrence, E. Spyropoulos, T.S.R. Reddy (NASA/TM ; 2000-209635)
マイクロ図書
2000<YCA-NAS 1.15:209635>
国立国会図書館
  • 件名Unsteady aerodynamics Computer programs Aerodynamic...

Methodology of blade unsteady pressure measurement in the NASA transonic flutter cascade [microform] / J. Lepicovsky ... [et al.] (NASA/TM ; 2002-211894)

Methodology of blade unsteady pressure measurement in the NASA transonic flutter cascade [microform] / J. Lepicovsky ... [et al.] (NASA/TM ; 2002-211894)
マイクロ図書
2002<YCA-NAS 1.15:2002-211894>
国立国会図書館
  • 件名Transonic flutter Unsteady aerodynamics Rotary wings Computerized sim...

Gust response analysis of a turbine cascade [microform] / R.S.R. Gorla ... [et al.] ([NASA technical memorandum] ; NASA/TM-2001-210562)

Gust response analysis of a turbine cascade [microform] / R.S.R. Gorla ... [et al.] ([NASA technical memorandum] ; NASA/TM-2001-210562)
マイクロ図書
2001<YCA-NAS 1.15:210562>
国立国会図書館
  • 件名Gusts Dynamic response Turbines Turbomachine blades Cascade flow Annular flow Unsteady aerodynamics

Unsteady aerodynamics [microform] : subsonic compressible inviscid case / A.V. Balakrishman ([NASA contractor report] ; NASA/CR-1999-206583)

Unsteady aerodynamics [microform] : subsonic compressible inviscid case / A.V. Balakrishman ([NASA contractor report] ; NASA/CR-1999-206583)
マイクロ図書
1999<YCA-NAS 1.26:206583>
国立国会図書館
  • 件名Inviscid flow Unsteady aerodynamics Subsonic flow Compressible fl...

Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation [microform] / Jensen Lin, Kenneth W. Iliff ([NASA technical memorandum] ; NASA/TM-2000-209019)

Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation [microform] / Jensen Lin, Kenneth W. Iliff ([NASA technical memorandum] ; NASA/TM-2000-209019)
マイクロ図書
2000<YCA-NAS 1.15:209019>
国立国会図書館
  • 件名...hod of moments Unsteady aerodynamics Laplace transformation

Modeling of unsteady three-dimensional flows in multistage machines [microform] / Kenneth C. Hall and Edmund T. Pratt

Modeling of unsteady three-dimensional flows in multistage machines [microform] / Kenneth C. Hall and Edmund T. Pratt
マイクロ図書
2003<YCA-NAS 1.26:2003-212101>
国立国会図書館
  • 件名Unsteady flow Unsteady aerodynamics Turbomachinery Applications p...

Analysis of inlet-compressor acoustic interactions using coupled CFD codes [microform] / A. Suresh ... [et al.] (NASA/TM ; 1998-208839)

Analysis of inlet-compressor acoustic interactions using coupled CFD codes [microform] / A. Suresh ... [et al.] (NASA/TM ; 1998-208839)
マイクロ図書
1998<YCA-NAS 1.15:208839>
国立国会図書館
  • 件名Computational fluid dynamics Turbomachinery Supersonic inlets Unsteady aerodynamics

Development of a composite tailoring technique for airplane wing [microform] : progress report/renewal proposal, grant no. NAG2-908 / principal investigator, Aditi Chattopadhyay ; graduate research associate, Ratneshwar Jha ([NASA contractor report] ; NASA CR-205326)

Development of a composite tailoring technique for airplane wing [microform] : progress report/renewal proposal, grant no. NAG2-908 / principal investigator, Aditi Chattopadhyay ; graduate research associate, Ratneshwar Jha ([NASA contractor report] ; NASA CR-205326)
マイクロ図書
1997<YCA-NAS 1.26:205326>
国立国会図書館
  • 件名...tural analysis Unsteady aerodynamics

Estimation of aircraft nonlinear unsteady parameters from wind tunnel data [microform] / Vladislav Klein, Patrick C. Murphy (NASA/TM ; 1998-208969)

Estimation of aircraft nonlinear unsteady parameters from wind tunnel data [microform] / Vladislav Klein, Patrick C. Murphy (NASA/TM ; 1998-208969)
マイクロ図書
1998<YCA-NAS 1.15:208969>
国立国会図書館
  • 件名Wind tunnel tests Unsteady aerodynamics Aerodynamic forces Mathematic...

Computational test cases for a rectangular supercritical wing undergoing pitching oscillations [microform] / Robert M. Bennett and Charlotte E. Walker ([NASA technical memorandum] ; NASA/TM-1999-209130)

Computational test cases for a rectangular supercritical wing undergoing pitching oscillations [microform] / Robert M. Bennett and Charlotte E. Walker ([NASA technical memorandum] ; NASA/TM-1999-209130)
マイクロ図書
1999<YCA-NAS 1.15:209130>
国立国会図書館
  • 件名Computational fluid dynamics Unsteady aerodynamics Rectangular wings Supercritic...

Active control of flow separation over an airfoil [microform] / S.S. Ravindran ([NASA technical memorandum] ; NASA/TM-1999-209838)

Active control of flow separation over an airfoil [microform] / S.S. Ravindran ([NASA technical memorandum] ; NASA/TM-1999-209838)
マイクロ図書
1999<YCA-NAS 1.15:209838>
国立国会図書館
  • 件名...Separated flow Unsteady aerodynamics

Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques [microform] / Walter A. Silva

Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques [microform] / Walter A. Silva
マイクロ図書
1997<YCA-NAS 1.15:112832>
国立国会図書館
  • 件名...fluid dynamics Unsteady aerodynamics Aeroelasticity

Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data [microform] / Vladislav Klein and Patrick C. Murphy (NASA/TM ; 97-207993)

Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data [microform] / Vladislav Klein and Patrick C. Murphy (NASA/TM ; 97-207993)
マイクロ図書
1998<YCA-NAS 1.15:207993>
国立国会図書館
  • 件名... X-31 aircraft Unsteady aerodynamics Supersonic aircraft Fighter a...

Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines [microform] / Om P. Sharma ... [et al.] (NASA contractor report ; 202319)

Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines [microform] / Om P. Sharma ... [et al.] (NASA contractor report ; 202319)
マイクロ図書
1997<YCA-NAS 1.26:202319>
国立国会図書館
  • 件名...low Axial flow Unsteady aerodynamics Navier-Stokes equation Comput...

Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques [microform] / Walter A. Silva (NASA technical memorandum ; 112872)

Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques [microform] / Walter A. Silva (NASA technical memorandum ; 112872)
マイクロ図書
1997<YCA-NAS 1.15:112872>
国立国会図書館
  • 件名...Linear systems Unsteady aerodynamics

System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality [microform] : a dissertation ... / by Ralph David Buehrle (NASA-TM ; 112690)

System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality [microform] : a dissertation ... / by Ralph David Buehrle (NASA-TM ; 112690)
マイクロ図書
1997<YCA-NAS 1.15:112690>
国立国会図書館
  • 件名... tunnel models Unsteady aerodynamics Equations of motion Angle of ...

Analysis of wind tunnel oscillatory data of the X-31A aircraft [microform] / Mark S. Smith ([NASA contractor report] ; NASA/CR-1999-208725)

Analysis of wind tunnel oscillatory data of the X-31A aircraft [microform] / Mark S. Smith ([NASA contractor report] ; NASA/CR-1999-208725)
マイクロ図書
1999<YCA-NAS 1.26:208725>
国立国会図書館
  • 件名...atic stability Unsteady aerodynamics Mathematical models

Computational aeroservoelastic analysis with an Euler-based unsteady flow solver [microform] : NASA-Ames university consortium cooperative agreement no. NCC2-5105, final research summary for the period: 1 November 1994 - 31 January 1997 / principal investigator, Andrew S. Arena, Jr ([NASA contractor report] ; NASA-CR-203303)

Computational aeroservoelastic analysis with an Euler-based unsteady flow solver [microform] : NASA-Ames university consortium cooperative agreement no. NCC2-5105, final research summary for the period: 1 November 1994 - 31 January 1997 / principal investigator, Andrew S. Arena, Jr ([NASA contractor report] ; NASA-CR-203303)
マイクロ図書
1997<YCA-NAS 1.26:203303>
国立国会図書館
  • 件名Aeroservoelasticity Unsteady aerodynamics Finite element method Mach nu...

An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation [microform] / W. Keats Wilkie, K.C. Park (NASA technical memorandum ; 110252)

An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation [microform] / W. Keats Wilkie, K.C. Park (NASA technical memorandum ; 110252)
マイクロ図書
1996<YCA-NAS 1.15:110252>
国立国会図書館
  • 件名...s Rotary wings Unsteady aerodynamics Differential equations Galerk...
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