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↗
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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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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↗
Effect of body nose blunting, control planform area, and leading-edge bluntness on aerodynamic control of a 5 deg semivertex cone at Mach number 6.9
Effect of body nose blunting, control planform area, and leading edge bluntness on aerodynamic control of semivertex cone at hypersonic speed
HYPERSONIC SPEED↗
Measurements of the Mach number and pressure on the afterbody of a blunt-nosed model in free flight at Mach numbers from 6.5 to 14
Mach number and pressure measurements on afterbody of blunt-nose model in free flight at hypersonic speeds
MACH NUMBER↗
A wind-tunnel investigation of the dynamic stability of axisymmetric models with hammerhead noses in transonic flow
Wind tunnel investigation of dynamic stability of axisymmetric models with hammerhead noses
DYNAMIC STABILITY↗
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 km per second
STATIC STABILITY↗
Effects of angle of attack and nose bluntness on the hypersonic flow over cones.
Nose bluntness and angle of attack effects on hypersonic flow, noting shock wave deflection decrease of minimum possible shock angle, varying specific heat ratio, convective heating, boundary layer transition, etc
SPECIFIC HEAT↗
Interaction effects of a control jet exhausting radially from the nose of an ogive- cylinder body at transonic speeds
Interaction effects of control jet exhausting radially from nose of ogive-cylinder body at transonic speeds
TRANSONIC SPEED↗
Force measurements on axisymmetric models with hammerhead noses at transonic speeds
Normal-force, pitching-moment and axial-force coefficients for axisymmetry models with hammerhead noses at transonic speeds in wind tunnel
HAMMERHEAD CONFIGURATION↗
Centaur/Surveyor nose fairing aerodynamic heating investigation
Aerodynamic heating, delamination and pressure in nose fairing honeycomb core of Atlas Centaur launch vehicle
Eastwood, C. W., Jr.↗
Effects of nose shape and fin geometry on static stability of a high-fineness-ratio sounding rocket
Nose shape and fin geometry effects on static stability of sounding rocket models in supersonic wind tunnel
Fuller, D. E.↗
Effects of variations in nose and windshield geometry on supersonic aerodynamic characteristics of a variable-sweep tactical fighter model
Windshield and nose geometry effects on supersonic aerodynamic characteristics of tactical fighter model
Richardson, C. S.↗
Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5 deg half-angle cone at Mach 8
Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on 5 degree half-angle cone at Mach 8
Stainback, P. C.↗
Aerodynamic loads on deployed canard surfaces and rocket nose section of the Apollo launch escape vehicle
Aerodynamic loads on deployed canard surfaces and rocket nose section of Apollo launch escape vehicle
Moseley, W. C., Jr.↗
Analysis of dynamic jettison hinge forces for Centaur nose fairing
Performance tests on dynamic jettison hinge loads of Centaur nose fairing
Tang, H. M.↗
Combined effects of mass addition and nose bluntness on boundary-layer transition.
Cone boundary layer transition location and Reynolds number as function of nose bluntness combined effect with Ar, air and He mass injection
Akin, C. M.↗