ADVANCED STATIC INVERTER UTILIZING DIGITAL TECHNIQUES AND HARMONIC CANCELLATION
Advanced static inverter utilizing digital techniques and harmonic cancellation
ELECTRONICS↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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STATIC STABILITY INVESTIGATION OF PROPOSED PROJECT FIRE SPACE-VEHICLE AND REENTRY-PACKAGE CONFIGURATIONS AT MACH NUMBERS FROM 1.47 TO 4.63
Project fire - space and reentry vehicle static stability
REENTRY VEHICLE↗
Propeller Slipstream Effects As Determined From Wing Pressure Distribution Of A Large-Scale Six-Propeller VTOL Model At Static Thrust
Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-propeller vtol model at static thrust
STATIC THRUST↗
STATIC STABILITY TESTS IN THE LANGLEY 24-INCH HYPERSONIC ARC TUNNEL ON A BLUNTED CONE AT A MACH NUMBER OF 20
Static stability tests in hypersonic arc tunnel on blunted cone at mach 20
BLUNT BODY↗
FREE-FLIGHT MEASUREMENTS OF DRAG AND STATIC STABILITY FOR A BLUNT-NOSED 10 DEG HALF-ANGLE CONE AT MACH NUMBER 15
Drag and static stability for a blunt-nosed 10-deg half-angle cone in hypersonic free-flight
STATIC STABILITY↗
THEORY AND IMPLEMENTATION OF THE PITOT-STATIC TECHNIQUE FOR UPPER ATMOSPHERIC MEASUREMENTS
Pitot-static technique for upper atmospheric measurements
ATMOSPHERIC COMPOSITION↗
INVESTIGATION OF STATIC PRESSURES AND BOUNDARY-LAYER CHARACTERISTICS ON THE FORWARD PARTS OF NINE FUSELAGES OF VARIOUS CROSS-SECTIONAL SHAPES AT M INFINITY EQUAL 2.01
Boundary layer characteristics of fuselages of various cross sectional shapes at static pressure
FUSELAGE↗
STATIC STABILITY AND CONTROL CHARACTERISTICS OF AN AIRPLANE MODEL WITH TAIL SURFACES OUTBOARD OF THE WING TIPS AT A MACH NUMBER OF 2.01
Static stability and control characteristics of aircraft model with tail surfaces outboard of wing tips
SUPERSONIC SPEED↗
STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG
Static longitudinal aerodynamics of wing and blunt body shapes for use as reentry configurations at hypersonic speed and angles of attack up to 90-deg
HYPERSONIC SPEED↗
THE LOW-SPEED STATIC LONGITUDINAL AND LATERAL-CHARACTERISTICS OF A DELTA-WING MODEL WITH FIXED AND FREE-FLOATING CANARD SURFACES
Low-speed static longitudinal and lateral characteristics of delta-wing model with fixed and free-floating canard surfaces
LONGITUDINAL STABILITY↗
STATIC LONGTIDUDINAL STABILITY CHARACTERISTICS OF A BLUNTED GLIDER REENTRY CONFIGURATION HAVING 79.5 DEG SWEEPBACK AND 45 DEG DIHEDRAL AT A MACH NUMBER OF 6.2 AND ANGLES OF ATTACK UP TO 20 DEG
Static longitudinal stability characteristics of blunted glider reentry configuration
LONGITUDINAL STABILITY↗
WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER
Wind tunnel investigation at subsonic & transonic speed of static aerodynamic and control characteristics of capsule-booster model
CONTROL↗
Aerodynamic Performance and Static Stability at Mach Numbers of Up to 5 of Two Airplane Configurations with Favorable LIft interference
Performance and static stability of supersonic aircraft configuration with lift interference
LIFT↗
STATIC LONGITUDINAL AND LATERAL STABILITY CHARACTERISTICS AT A MACH NUMBER OF 3.11 OF SQUARE AND CIRCULAR PLAN-FORM REENTRY VEHICLES, WITH SOME EFFECTS OF CONTROLS AND LEADING-EDGE EXTENSIONS
Static stability of square and circular planform reentry vehicles at mach 3.11 - effects of controls and leading-edge extensions
STATIC STABILITY↗
WIND-TUNNEL INVESTIGATION OF THE STATIC STABILITY OF A 1 56-SCALE MODEL OF THE X-1E AIRPLANE AT MACH NUMBERS OF 2.37, 2.98, AND 4.01
Wind tunnel tests of static stability of model x-1e aircraft at mach 2 to 4
X-1 AIRCRAFT↗
TRANSONIC STATIC AERODYNAMIC CHARACTERISTICS OF A BLUNT CONECYLINDER BODY WITH FLARED AFTERBODIES OF VARIOUS ANGLES AND BASE AREAS
Transonic static aerodynamic characteristics of blunt cone cylinder body with flared afterbodies of various angles and base areas
AFTERBODY↗
Static Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Lenticular-Shaped Reentry Vehicle
Lenticular-shaped reentry vehicle static longitudinal aerodynamic characteristics at transonic speeds
REENTRY VEHICLE↗
STATIC STABILITY AND CONTROL CHARACTERISTICS AT LOW-SUBSONIC SPEEDS OF A LENTICULAR REENTRY CONFIGURATION
Static stability and control characteristics of manned lenticular reentry configuration at low subsonic speeds
STATIC STABILITY AND CONTROL↗