SHOCK-WAVE PROFILES OVER ELLIPSOIDAL-NOSED BODIES IN HYPERSONIC FLOW
Shock-wave profiles over ellipsoidal-nosed bodies in hypersonic flow
ELLIPSOID↗
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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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LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT LOW SUBSONIC SPEEDS OF A HIGHLY SWEPT DELTA WING UTILIZING NOSE DEFLECTION FOR CONTROL
Longitudinal aerodynamic characteristics at low subsonic speeds of a highly swept delta wing with nose deflection control
SWEPT WING↗
SHOCK-WAVE PROFILES OVER ELLIPSOIDAL-NOSED BODIES IN SUPERSONIC FLOW
Shock wave profiles of ellipsoidal-nosed bodies in supersonic flow
SHOCK WAVE↗
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↗
Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack up to 180 Deg
Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics of blunt bodies
AERODYNAMIC CHARACTERISTICS↗
HEAT-TRANSFER MEASUREMENTS ON A CONCAVE HEMISPHERICAL NOSE SHAPE WITH UNSTEADY-FLOW EFFECTS AT MACH NUMBERS OF 1.98 AND 4.95
Heat transfer on concave hemispherical nose shape with unsteady flow effect
HEMISPHERE↗
BLAST-WAVE CORRELATION OF PRESSURES ON BLUNT-NOSED CYLINDERS IN PERFECT AND REAL-GAS FLOWS AT HYPERSONIC SPEEDS
Equation from blast wave correlation of pressures on blunt nosed cylinders in perfect and real gas flows at hypersonic speeds
BLUNT BODY↗
Blast-wave correlation of pressures on blunt- nosed cylinders in perfect- and real-gas flows at hypersonic speeds.
Blast-wave correlation of pressures on blunt-nosed cylinders in perfect and real-gas flow at hypersonic speeds
SHOCK WAVE↗
Calculated radio attenuation due to plasma sheath of hypersonic blunt-nosed cone
Calculated radio attenuation due to plasma sheath on hypersonic blunt-nosed cone
BLUNT BODY↗
Some measurements of the dynamic and static stability of two blunt-nosed, low-fineness- ratio bodies of revolution in free flight at mequal4
Dynamic and static stability of two blunt nosed low fineness ratio bodies of revolution in free flight - ballistics
STATIC STABILITY↗
A parametric study of the aerodynamic charac- teristics of nose-cylinder-flare bodies at a mach number of 6.0
Longitudinal aerodynamic characteristics of nose cylinder-flare reentry bodies measured in hypersonic wind tunnel
LONGITUDINAL STABILITY↗
Flight evaluation of the x-15 ball-nose flow-direction sensor as an air-data system
Modification of ball-nose flow direction sensor for Mach number and air pressure altitude measurements
PRESSURE MEASUREMENT↗
The pressure profile of a rocket payload after nose-cone ejection
Pressure measurement at instrument rack of sounding rocket payload after nose cone ejection
INSTRUMENTATION↗
A description of numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over blunt-nosed and flared bodies
Numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over blunt-nosed and flared bodies
AXISYMMETRIC FLOW↗
On the direct shock wave problem. a modified theory /final report on bodies with spherical nose/
Modification of mathematical approach to general body problem for investigating direct shock wave problem for bodies with spherical nose
SHOCK WAVE↗
Free-flight tests of a blunt-nosed flare- stabilized body at speeds to 8.2 km/sec.
Static and dynamic stability and drag of blunt- nosed flare-stabilized bodies at velocities up to 8.2 kilometers per second
FLARED BODY↗
Effect of nose-mounted control-system jets in roll-control positions on the aerodynamics of a space vehicle
Nose-mounted control-system jets in roll-control positions effect on aerodynamics of space vehicle
CONTROL SYSTEM↗
Flight demonstration of a nose-mounted rotating-solid-propellant rocket control system and a comparison with analog studies
Flight test of nose mounted rotating solid propellant rocket attitude control system for space vehicle second stage
ATTITUDE CONTROL↗