IN-FLIGHT GAINS REALIZED BY MODIFYING A TWIN SIDE-INLET INDUCTION SYSTEM
Modification of twin side-inlet induction system and in-flight gains
INLET↗
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TESTS OF A TWIN-DUCT INDUCTION SYSTEM FOR A MACH NUMBER RANGE OF 0.78 TO 2.07
Flight tests of twin-duct induction system
DUCT↗
RESULTS OF STUDIES ON A TWIN-GYRO ATTITUDE CONTROL SYSTEM FOR SPACE VEHICLES
Automatic closed loop and pilot operated twin-gyro systems are discussed as attitude stabilizers for large space vehicles
GYRO-STABILIZED↗
Simulator study of precise attitude stabili- zation of a manned spacecraft by twin gyros and pulse-modulated reaction jets
Attitude stabilization of manned spacecraft by twin gyros and pulse-modulated reaction jets
REACTION JET↗
Results of studies on a twin-gyro attitude- control system for space vehicles
Twin gyroscopic control system for three orthogonal axes of space vehicle attitude control
GYROSCOPE↗
Lateral control characteristics of a powered model of a twin-propeller deflected slipstream stol airplane configuration
Wind tunnel tests of static lateral and directional control of twin-propeller deflected slipstream STOL aircraft
DEFLECTION↗
Blast effects of twin variable-cant rocket nozzles on visibility during landing on a particle-covered surface
Jet blast effect of twin variable cant rocket nozzles on visibility during landing on particle covered surface
ROCKET NOZZLE↗
Performance of Twin-duct Variable-geometry Side Inlets at Mach Numbers of 1.5 to 2.0
Supersonic wind tunnel test of twin-duct variable geometry side inlets
VARIABLE GEOMETRY STRUCTURE↗
An investigation of splitter plates for supersonic twin inlets
Ability of splitter plates to isolate twin inlets aerodynamically
SUPERSONIC INLET↗
Effects of Boattail Area Contouring and Simulated Turbojet Exhaust on the Loading and Fuselage-tail Component Drag of a Twin-engine Fighter-type Airplane Model
Effects of boattail area contouring and simulated turbojet exhaust on loading and fuselage-tail component drag of twin-engine fighter-type airplane model
AERODYNAMIC LOAD↗
An investigation of splitter plates for supersonic twin inlets
Splitter plates for aerodynamic isolation of supersonic twin inlets
SUPERSONIC FLOW INLET↗
Longitudinal stability and control characteristics of a powered model of a twin-propeller deflected-slipstream STOL AIRPLANE configuration
Longitudinal stability and control characteristics of powered model of twin-propeller deflected-slipstream STOL aircraft configuration
STOL AIRCRAFT↗
Effects of aft-fuselage-mounted nacelles on the subsonic longitudinal aerodynamic characteristics of a twin-turbojet airplane
Aft-fuselage-mounted nacelles effect on subsonic longitudnal aerodynamic characteristics of twin turbojet aircraft
SUBSONIC SPEED↗
Internal deformation and fracture of second order 1011-1012 twins in magnesium
Structural deformation, and fractures caused by second order twinning in magnesium single crystals
Hartt, W. H., III↗
Summary of VGH data collected on one type of twin-engine jet airplane during airline operations
Summary of vertical gusts acceleration data collected for one type twin engine jet airplane during airline operations
Brazziel, M. E.↗
Internal deformation and fracture of second- order /1011/-/1012/ twins in magnesium.
Internal deformation and fracture of second order /1011/-/1012/ twins in Mg single crystals, noting large strains
Hartt, W. H.↗
Full-scale wind-tunnel investigation of static longtudinal and lateral characteristics of a light twin-engine airplane
Full scale wind tunnel investigation of lateral and longitudinal stability and control characteristics of light twin engine airplane
Fink, M. P.↗
Wind-tunnel investigation of the aerodynamic characteristics of a twin-keel parawing
Wind tunnel investigation of twin keel parawing aerodynamic characteristics
Ware, G. M.↗