Effects of Coupling Between Pitch and Roll Control Inputs on the Handling Qualities of VTOL Aircraft
Effects of coupling between pitch and roll control inputs on handling qualities of vtol aircraft
STABILITY AND CONTROL↗
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THE EQUATORIAL PITCH ANGLE DISTRIBUTIONS OF ELECTRONS IN THE OUTER RADIATION BELT
Equatorial pitch angle distribution of electrons in the outer radiation belt
OUTER RADIATION BELT↗
THE ORIGIN AND DISTRIBUTION OF SUPERSONIC STORE INTERFERENCE FROM MEASUREMENT OF INDIVIDUAL FORCES ON SEVERAL WING-FUSELAGE-STORE CONFIGURATIONS. II - SWEPT-WING HEAVY-BOMBER CONFIGURATION WITH LARGE STORE NACELLE. LATERAL FORCES AND PITCHING MOMENTS, MACH NUMBER, 1.61
Effect of large store /nacelle/ on a swept-wing heavy bomber - lateral force and pitching moments
SWEPT WING↗
WIND TUNNEL AND LABORATORY TESTS ON THE EDCLIFF 4-15 ANGLE OF PITCH AND YAW TRANSDUCER
Yaw & pitch angle transducer - wind tunnel & laboratory tests at transonic and supersonic speeds
PITCHING MOMENT↗
MEASUREMENT OF PITCH DAMPING AT LARGE ANGLES OF OSCILLATION FOR PROPOSED MARS ATMOSPHERE-ENTRY VEHICLES
Wind tunnel techniques used to determine pitch damping at large angles of oscillation for proposed mars atmospheric entry vehicles
DAMPING IN PITCH↗
Effect of Forebody Strakes on the Aerodynamic Characteristics in Pitch and Sideslip of a Hypersonic Airplane Configuration at Mach Numbers of 1.41, 2.01, and 6.86
Effect of forebody strakes on aerodynamic characteristics in sideslip and pitch of hypersonic aircraft configurations
PITCH ATTITUDE↗
Application of the pitch modulation maneuver in the region of the ''limiting'' entry velocity.
Pitch modulation maneuver for spacecraft reentry
SPACECRAFT REENTRY↗
Results of the JPL aerodynamic damping-in- pitch wind-tunnel program
Results on aerodynamic damping in pitch of spherical and conical models in high velocity wind tunnel
DYNAMIC MODEL↗
Aerodynamic damping and oscillatory stability in pitch for a model of a typical subsonic jet-transport airplane
Aerodynamic damping and oscillatory stability in pitch for model of typical swept wing subsonic jet transport
SWEPT WING↗
Aerodynamic damping and oscillatory stability in pitch and yaw of Gemini configurations at Mach numbers from 0.50 to 4.63
Aerodynamic damping and oscillatory stability in pitch and yaw of Gemini abort and reentry configurations at transonic and supersonic speeds
DAMPING IN YAW↗
Aerodynamic characteristics in pitch, including effects of horizontal-tail negative dihedral angle, of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds
Aerodynamic characteristics in pitch of horizontal attitude VTOL aircraft, including effects of negative dihedral horizontal tail
PITCHING MOMENT↗
Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75 deg
Aerodynamic characteristics in pitch of variable sweep V/STOL configurations tested in supersonic wind tunnel
AERODYNAMIC CHARACTERISTICS↗
A parametric study of factors influencing the deep-stall pitch-up characteristics of T-tail transport aircraft
Analog computer program for parametric study of factors influencing deep stall pitch-up characteristics of T-tail transport aircraft
STALLING↗
Low-speed wind-tunnel studies relating to pitch-up on a supersonic transport model with a high-aspect-ratio variable-sweep wing
Low speed wind tunnel testing of high aspect ratio variable sweep wing supersonic transport model for determining methods of reducing pitch-up tendency
PITCH CONTROL↗
Application of the pitch modulation maneuver in the region of the ''limiting'' entry velocity.
Pitch modulation maneuver for spacecraft reentry
PITCH CONTROL↗
Equations for the application of wind-tunnel wall corrections to pitching moments caused by the tail of an aircraft model
Mathematical expressions derived for application of wind tunnel wall corrections to pitching moments caused by tail of aircraft model
AIRCRAFT MODEL↗
Qualification evaluation of the pitch control motor for the launch escape system of the Apollo spacecraft program
Environmental testing and static firing of pitch control motor for Apollo spacecraft launch escape system
ESCAPE ROCKET↗
Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing
Flight simulator study of pitch maneuver speed margins for variable-sweep wing supersonic transport configuration
FLIGHT SIMULATION↗