EXPERIMENTAL SEA-LEVEL STATIC INVESTIGATION OF A SHORT AFTERBURNER
Sea-level static testing of turbojet engine afterburner
STATIC TESTING↗
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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 AERODYNAMIC CHARACTERISTICS OF A THREE-STAGE ROCKET VEHICLE HAVING VARIOUS FIN CONFIGURATIONS AT LOW SUBSONIC MACH NUMBERS AND ANGLES OF ATTACK UP TO 28 DEG
Static aerodynamic characteristics of three-stage trailblazer ii rocket vehicle determined in low turbulence pressure wind tunnel
TRAILBLAZER II REENTRY VEHICLE↗
EFFECT OF VERTICAL-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS
Effect of vertical tail modifications on static stability of vtol supersonic aircraft
SUPERSONIC AIRCRAFT↗
STATIC STABILITY AND CONTROL OF HYPERSONIC GLIDERS
Static stability and control of hypersonic gliders
STABILITY AND CONTROL↗
UPPER-ATMOSPHERE STRUCTURE MEASUREMENT MADE WITH THE PITOT-STATIC TUBE
Upper-atmosphere structure measurement made with pitot-static tube
UPPER ATMOSPHERE↗
Low-Speed Investigation Of The Effects Of Horizontal-Tail Area And Wing Sweep On The Static Longitudinal Stability And Control Characteristics Of An Airplane Configuration Having Tail Surfaces Outboard Of The Wing Tips
Low-speed longitudinal static stability & control characteristics of aircraft with swept wings & tail surfaces outboard of wing tips
STABILITY AND CONTROL↗
FREE-FLIGHT MEASUREMENTS OF STATIC AND DYNAMIC STABILITY OF MODELS OF THE PROJECT MERCURY RE-ENTRY CAPSULE AT MACH NUMBERS 3 AND 9.5
Static & dynamic stability of mercury reentry capsule scale models at mach 3 & 9.5
REENTRY VEHICLE↗
WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.30 TO 1.14 OF THE STATIC AERODYNAMIC CHARACTERISTICS OF MODIFIED MERCURY ESCAPE AND EXIT CAPSULE CONFIGURATIONS
Static aerodynamic characteristics of modified mercury escape and exit capsule configurations at mach numbers 0.30 to 1.4
MERCURY CAPSULE↗
EXPERIMENTAL STUDIES OF STATIC STABILITY AND RADIATIVE HEATING ASSOCIATED WITH MARS AND VENUS ENTRY
Experimental studies of radiative heating and static stability in relation to vehicle entry into the atmospheres of mars and venus
RADIATIVE HEAT TRANSFER↗
Experimental studies of static stability and radiative heating associated with mars and venus entry
Static stability and radiative heating associated with mars and venus atmospheric entry
STATIC STABILITY↗
Residual static strength of several titanium and stainless-steel alloys and one superalloy at -109 deg. f, 70 deg. f, and 550 deg. f
Residual static strength of titanium & stainless steel alloys and one superalloy at various temperatures
STATIC STABILITY↗
The prediction of notch and crack strength under static or fatigue loading
Notch and crack strength of metals under static or fatigue loading
FATIGUE↗
Effects of gross changes in static directional stability on v/stol handling characteristics based on a flight investigation
Helicopter flight investigation of effects of gross changes in static directional stability on v/stol handling
HELICOPTER↗
Comparisons of experimental with predicted wall static-pressure distributions in conical supersonic nozzles
Experimental and predicted wall static-pressure distributions in conical supersonic nozzles
CONICAL NOZZLE↗
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↗
The static stability characteristics of several preliminary models of the x-15 research airplane at mach numbers of 2.98 and 4.01
Static stability characteristics of preliminary models of X-15 research aircraft at supersonic speeds
STATIC STABILITY↗
High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0 deg to 90 deg
High subsonic speed of static longitudinal aerodynamic characteristics of delta wing configuration for angle of attack from 0 deg to 90 deg
DELTA WING↗
An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers from 3.0 to 6.3
Static longitudinal stability and control characteristics of wingless missile configuration at supersonic and hypersonic speeds
WINGLESS VEHICLE↗