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Forebody flow visualization on the F-18 HARV with actuated forebody strakes [microform] / David F. Fisher and Daniel G. Murri ([NASA technical memorandum] ; NASA/TM-1998-206556)

Forebody flow visualization on the F-18 HARV with actuated forebody strakes [microform] / David F. Fisher and Daniel G. Murri ([NASA technical memorandum] ; NASA/TM-1998-206556)
マイクロ図書
1998<YCA-NAS 1.15:206556>
国立国会図書館
  • 件名Flow visualization F-18 aircraft Forebodies Pressure measureme...

An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data [microform] / Candida D. Olney and Heather Hillebrandt, Eric Y. Reichenbach (NASA/TM ; 2000-209028)

An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data [microform] / Candida D. Olney and Heather Hillebrandt, Eric Y. Reichenbach (NASA/TM ; 2000-209028)
マイクロ図書
2000<YCA-NAS 1.15:209028>
国立国会図書館
  • 件名Aeroelasticity Wing loading F-18 aircraft Aircraft models Flight tests ...

Advances in experiment design for high performance aircraft [microform] : paper no. 8 / Engene A. Morelli (NASA/TM ; 207994)

Advances in experiment design for high performance aircraft [microform] : paper no. 8 / Engene A. Morelli (NASA/TM ; 207994)
マイクロ図書
1998<YCA-NAS 1.15:207994>
国立国会図書館
  • 件名Supersonic aircraft Research vehicles Cramer-Rao bounds F-18 aircraft

Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang ([NASA technical paper] ; NASA/TP-1999-206573)

Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang ([NASA technical paper] ; NASA/TP-1999-206573)
マイクロ図書
1999<YCA-NAS 1.60:206573>
国立国会図書館
  • 件名F-18 aircraft Angle of attack Maximum likel...

Nonclassical flight control for unhealthy aircraft [microform] : final report : (March 28, 1997-November 30, 1997) / prepared by Ping Lu ([NASA contractor report] ; 206660)

Nonclassical flight control for unhealthy aircraft [microform] : final report : (March 28, 1997-November 30, 1997) / prepared by Ping Lu ([NASA contractor report] ; 206660)
マイクロ図書
1997<YCA-NAS 1.26:206660>
国立国会図書館
  • 件名Control equipment Aircraft control Flight tests Flight control F-18 aircraft Damage

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft [microform] / W.G. Steenken ... [et al.] (NASA/TM ; 1999-206572)

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft [microform] / W.G. Steenken ... [et al.] (NASA/TM ; 1999-206572)
マイクロ図書
1999<YCA-NAS 1.15:206572>
国立国会図書館
  • 件名F-18 aircraft Aerodynamic stability Angle o...

Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails [microform] : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV / Robert W. Moses, Holt Ashley (NASA/TM ; 1998-207323)

Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails [microform] : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV / Robert W. Moses, Holt Ashley (NASA/TM ; 1998-207323)
マイクロ図書
1998<YCA-NAS 1.15:207323>
国立国会図書館
  • 件名...tack Buffeting F-18 aircraft Leading edges Turbulent wakes...

Evaluation of gritting strategies for high angle of attack using wind tunnel and flight test data for the F/A-18 [microform] / Robert M. Hall ... [et al.] ([NASA technical paper] ; NASA/TP-1998-207670)

Evaluation of gritting strategies for high angle of attack using wind tunnel and flight test data for the F/A-18 [microform] / Robert M. Hall ... [et al.] ([NASA technical paper] ; NASA/TP-1998-207670)
マイクロ図書
1998<YCA-NAS 1.60:207670>
国立国会図書館
  • 件名Angle of attack Flight tests Wind tunnel tests Flight characteristics Boundary layers F-18 aircraft

Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0⁰ to 70⁰ [microform] / Scott C. Asbury and Francis J. Capone (NASA technical paper ; 3531)

Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0⁰ to 70⁰ [microform] / Scott C. Asbury and Francis J. Capone (NASA technical paper ; 3531)
マイクロ図書
1995<YCA-NAS 1.60:3531>
国立国会図書館
  • 件名F-18 aircraft Thrust vector control Researc...

CFL3D, its history and some recent applications [microform] / Christopher I. Rumsey, Robert T. Biedron, and James L. Thomas (NASA technical memorandum ; 112861)

CFL3D, its history and some recent applications [microform] / Christopher I. Rumsey, Robert T. Biedron, and James L. Thomas (NASA technical memorandum ; 112861)
マイクロ図書
1997<YCA-NAS 1.15:112861>
国立国会図書館
  • 件名...ms (Computers) F-18 aircraft

Fiber optic experience with the smart actuation system on the F-18 systems research aircraft [microform] / Eddie Zavala (NASA/TM ; 97-206223)

Fiber optic experience with the smart actuation system on the F-18 systems research aircraft [microform] / Eddie Zavala (NASA/TM ; 97-206223)
マイクロ図書
1997<YCA-NAS 1.15:206223>
国立国会図書館
  • 件名Fiber optics Actuators F-18 aircraft Research aircraft Electromagn...

Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60⁰ angle of attack [microform] : contract NAS 3-26617 / Kevin R. Walsh ... [et al.] (NASA technical memorandum ; 104329)

Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60⁰ angle of attack [microform] : contract NAS 3-26617 / Kevin R. Walsh ... [et al.] (NASA technical memorandum ; 104329)
マイクロ図書
1997<YCA-NAS 1.15:104329>
国立国会図書館
  • 件名F-18 aircraft Angle of attack Aerodynamic c...

Production support flight control computers [microform] : research capability for F/A-18 aircraft at Dryden Flight Research Center / John F. Carter (NASA/TM ; 97-206233)

Production support flight control computers [microform] : research capability for F/A-18 aircraft at Dryden Flight Research Center / John F. Carter (NASA/TM ; 97-206233)
マイクロ図書
1997<YCA-NAS 1.15:206233>
国立国会図書館
  • 件名F-18 aircraft Airborne/spaceborne computers...

Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft [microform] / Martin J. Brenner (NASA technical paper ; 3647)

Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft [microform] / Martin J. Brenner (NASA technical paper ; 3647)
マイクロ図書
1996<YCA-NAS 1.60:3647>
国立国会図書館
  • 件名...ration damping F-18 aircraft

Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV [microform] / David F. Fisher, Daniel G. Murri, and Wendy R. Lanser (NASA technical memorandum ; 4774)

Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV [microform] / David F. Fisher, Daniel G. Murri, and Wendy R. Lanser (NASA technical memorandum ; 4774)
マイクロ図書
1996<YCA-NAS 1.15:4774>
国立国会図書館
  • 件名Angle of attack F-18 aircraft Aerodynamics Leading edges St...

A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane [microform] / Frederick J. Lallman, John B. Davidson, and Patrick C. Murphy ([NASA technical paper] ; NASA/TP-1998-208464)

A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane [microform] / Frederick J. Lallman, John B. Davidson, and Patrick C. Murphy ([NASA technical paper] ; NASA/TP-1998-208464)
マイクロ図書
1998<YCA-NAS 1.60:208464>
国立国会図書館
  • 件名...ngle of attack F-18 aircraft

An overview of the NASA F-18 High Alpha Research Vehicle [microform] / Albion H. Bowers ... [et al.] (NASA technical memorandum ; 4772)

An overview of the NASA F-18 High Alpha Research Vehicle [microform] / Albion H. Bowers ... [et al.] (NASA technical memorandum ; 4772)
マイクロ図書
1996<YCA-NAS 1.15:4772>
国立国会図書館
  • 件名F-18 aircraft Angle of attack Thrust vector...

Modeling of aircraft unsteady aerodynamic characteristics. Part 3, Parameters estimated from flight data [microform] / Vladislav Klein and Keith D. Noderer (NASA technical memorandum ; 110259)

Modeling of aircraft unsteady aerodynamic characteristics. Part 3, Parameters estimated from flight data [microform] / Vladislav Klein and Keith D. Noderer (NASA technical memorandum ; 110259)
マイクロ図書
1996<YCA-NAS 1.15:110259>
国立国会図書館
  • 件名X-31 aircraft F-18 aircraft Aerodynamic characteristics U...

High-alpha research vehicle lateral-directional control law description, analyses, and simulation results [microform] / John B. Davidson ... [et al.] ([NASA technical paper] ; NASA/TP-1998-208465)

High-alpha research vehicle lateral-directional control law description, analyses, and simulation results [microform] / John B. Davidson ... [et al.] ([NASA technical paper] ; NASA/TP-1998-208465)
マイクロ図書
1998<YCA-NAS 1.60:208465>
国立国会図書館
  • 件名...vector control F-18 aircraft

Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang (NASA technical memorandum ; 4786)

Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang (NASA technical memorandum ; 4786)
マイクロ図書
1997<YCA-NAS 1.15:4786>
国立国会図書館
  • 件名...identification F-18 aircraft Research vehicles Maximum lik...
  • 並列タイトル等（連結）... for the basic F-18 aircraft at high angles of attack
  • 並列タイトル等... for the basic F-18 aircraft at high angles of attack
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