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vstol aircraft

1-24 of 28 Books

View Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests By Helen E. Kourous

Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests

Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests

By Helen E. Kourous

View Computer simulation of a pilot in V/STOL aircraft control loops By William G. Vogt

Computer simulation of a pilot in V/STOL aircraft control loops

Computer simulation of a pilot in V/STOL aircraft control loops

By William G. Vogt

View Research on a two-dimensional inlet for a supersonic V/STOL propulsion system By J. L. Mark

Research on a two-dimensional inlet for a supersonic V/STOL propulsion system

Research on a two-dimensional inlet for a supersonic V/STOL propulsion system

By J. L. Mark

View Analysis of internal flow in a ventral nozzle for STOVL aircraft By C. Frederic Smith

Analysis of internal flow in a ventral nozzle for STOVL aircraft

Analysis of internal flow in a ventral nozzle for STOVL aircraft

By C. Frederic Smith

View A modeling technique for STOVL ejector and volume dynamics By Colin K. Drummond

A modeling technique for STOVL ejector and volume dynamics

A modeling technique for STOVL ejector and volume dynamics

By Colin K. Drummond

View The attributes of a variable-diameter rotor system applied to civil tiltrotor aircraft By Scott Brender

The attributes of a variable-diameter rotor system applied to civil tiltrotor aircraft

The attributes of a variable-diameter rotor system applied to civil tiltrotor aircraft

By Scott Brender

View Wind tunnel wall interference in V/STOL and high lift testing By Marie H. Tuttle

Wind tunnel wall interference in V/STOL and high lift testing

Wind tunnel wall interference in V/STOL and high lift testing

By Marie H. Tuttle

View Supersonic flow computations for an ASTOVL aircraft configuration By Sekaripuram Ramakrishnan

Supersonic flow computations for an ASTOVL aircraft configuration

Supersonic flow computations for an ASTOVL aircraft configuration

By Sekaripuram Ramakrishnan

View Aerodynamics of wing-slipstream interaction By N. D. Ellis

Aerodynamics of wing-slipstream interaction

Aerodynamics of wing-slipstream interaction

By N. D. Ellis

View Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft By Jack G. McArdle

Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft

Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft

By Jack G. McArdle

View Multiple-purpose subsonic naval aircraft (MPSNA) By D. M. Winkeljohn

Multiple-purpose subsonic naval aircraft (MPSNA)

Multiple-purpose subsonic naval aircraft (MPSNA)

By D. M. Winkeljohn

View Cooperative control theory and integrated flight and propulsion control By D. K. Schmidt

Cooperative control theory and integrated flight and propulsion control

Cooperative control theory and integrated flight and propulsion control

By D. K. Schmidt

View Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover By James A. Franklin

Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover

Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover

By James A. Franklin

View V/STOL dynamics, control, and flying qualities By James A. Franklin

V/STOL dynamics, control, and flying qualities

V/STOL dynamics, control, and flying qualities

By James A. Franklin

View V/STOL community annoyance due to noise By G. W. Johnston

V/STOL community annoyance due to noise

V/STOL community annoyance due to noise

By G. W. Johnston

View Integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques By Sanjay Garg

Integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques

Integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques

By Sanjay Garg

View V/STOL aircraft configurations and opportunities in the Pacific Basin By James A. Albers

V/STOL aircraft configurations and opportunities in the Pacific Basin

V/STOL aircraft configurations and opportunities in the Pacific Basin

By James A. Albers

View An experimental and theoretical investigation of propellers operating in turbulence By T. A. P. S. AppaRao

An experimental and theoretical investigation of propellers operating in turbulence

An experimental and theoretical investigation of propellers operating in turbulence

By T. A. P. S. AppaRao

View A method for the estimation of flight path perturbations during steep descents of V/STOL aircraft By B. Etkin

A method for the estimation of flight path perturbations during steep descents of V/STOL aircraft

A method for the estimation of flight path perturbations during steep descents of V/STOL aircraft

By B. Etkin

View A study of short haul air transportation for the southern Ontario transportation for the southern Ontario region in the year 1980 By David K. S. Yue

A study of short haul air transportation for the southern Ontario transportation for the southern Ontario region in the year 1980

A study of short haul air transportation for the southern Ontario transportation for the southern Ontario region in the year 1980

By David K. S. Yue

View Characteristics of a rectangular wing with a peripheral jet in ground effect By Karl Dau

Characteristics of a rectangular wing with a peripheral jet in ground effect

Characteristics of a rectangular wing with a peripheral jet in ground effect

By Karl Dau

View STOL-V/STOL city center transport aircraft study By McDonnell Aircraft Corporation

STOL-V/STOL city center transport aircraft study

STOL-V/STOL city center transport aircraft study

By McDonnell Aircraft Corporation

View Simulation evaluation of the control system command monitoring concept for the NASA V/STOL Research Aircraft (VSRA) By J. A. Schroeder

Simulation evaluation of the control system command monitoring concept for the NASA V/STOL Research Aircraft (VSRA)

Simulation evaluation of the control system command monitoring concept for the NASA V/STOL Research Aircraft (VSRA)

By J. A. Schroeder

View Characteristics of a rectangular wing with a peripheral jet in ground effect By James M. Davis

Characteristics of a rectangular wing with a peripheral jet in ground effect

Characteristics of a rectangular wing with a peripheral jet in ground effect

By James M. Davis