UNT Libraries Government Documents Department - 22 Matching Results

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Primary view of Altitude performance of J71-A-2(600-D1) turbojet engine
Smith, Ivan D. & Sivo, Joseph N.
December 28, 1956
Primary view of Component performance of J71-A-2(600-D1) turbojet engine at several Reynolds number indices
Seashore, Ferris L. & Corrington, Lester C.
December 28, 1956
Primary view of Evaluation of Liquefied Hydrocarbon Gases as Turbojet Fuels
Hibbard, Robert R.
December 28, 1956
Primary view of Performance of a blunt-lip side inlet with ramp bleed, bypass, and a long constant-area duct ahead of the engine : Mach number 0.66 and 1.5 to 2.1
Allen, John L.
December 28, 1956
Primary view of Performance of a Blunt-lip Side Inlet With Ramp Bleed, Bypass, and a Long Constant-area Duct Ahead of the Engine- Mach Numbers 0.66 and 1.5 to 2.1
Allen, John L.
December 28, 1956
Primary view of Wind-Tunnel Investigation of the Interference Effects during Separation of a 1/40-Scale Model Convair B-58 Airplane and Store at Mach Numbers of 1.41, 1.61, and 2.01
Driver, Cornelius
December 28, 1956
Primary view of Effect of a Fuselage on the Low-Speed Longitudinal Aerodynamic Characteristics of a 45 Degree Sweptback Wing with Double Slotted Flaps
Naeseth, Rodger L.
September 28, 1956
Primary view of Experimental Investigation of a Transonic Axial-Flow-Compressor Rotor Designed for Sonic Inlet Velocity with an Inlet Hub-Tip Radius of 0.35
Boxer, Emanuel & Bernot, Peter T.
September 28, 1956
Primary view of Free-flight investigation over a Mach number range from 0.74 to 1.43 at lift coefficients from minus 0.15 to 0.75 of an airplane-configuration model having a 52.5 degree delta wing and a low swept horizontal tail
Kehlet, Alan B.
September 28, 1956
Primary view of Supersonic Investigation of the Lift, Drag, Static Stability, and Hinge-Moment Characteristics of a Rocket-Powered Model of a Ballistic-Missile Configuration
Gillespie, Warren, Jr.
September 28, 1956
Primary view of Supersonic Investigation of the Lift, Drag, Static Stability, and Hinge-Moment Characteristics of a Rocket-Powered Model of a Ballistic-Missile Configuration
Gillespie, Warren, Jr.
September 28, 1956
Primary view of Free-flight Investigation at Transonic Speeds of the Stability Characteristics of a Tailless Missile Configuration Having a 45 Deg Sweptback Wing of Aspect Ratio 4
Arbic, Richard G.
August 28, 1956
Primary view of Free-Flight Investigation at Transonic Speeds of the Stability Characteristics of a Tailless Missile Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 4
Arbic, Richard G.
August 28, 1956
Primary view of Hinge Moment and Effectiveness of an Unswept Constant-Chord Control and an Overhang-Balanced, Swept Hinge-Line Control on an 80 Degree Swept Pointed Wing at Mach Numbers from 0.75 to 1.96
Guy, Lawrence D.
August 28, 1956
Primary view of Attenuation of Tangential-Pressure Oscillations in a Liquid-Oxygen-n-Heptane Rocket Engine With Longitudinal Fins
Priem, Richard J.
June 28, 1956
Primary view of Attenuation of tangential-pressure oscillations in a liquid-oxygen - n-heptane rocket engine with longitudinal fins
Priem, Richard J.
June 28, 1956
Primary view of A Bibliography of NACA Reports on Control of Turbojet Engines
Sanders, John C.
June 28, 1956
Primary view of Experimental and analytical investigation of an acceleration regulating control for a turbojet engine
Stiglic, Paul M.; Heppler, Herbert & Novik, David
June 28, 1956
Primary view of Full-Scale Evaluation of Some Flameholder Design Concepts for High-Inlet-Velocity Afterburners
Prince, William R.; Velie, Wallace W. & Braithwaite, Willis M.
June 28, 1956
Primary view of Full-scale evaluation of some flameholder design concepts for high-inlet-velocity afterburners
Prince, William R.; Velie, Wallace W. & Braithwaite, Willis M.
June 28, 1956
Primary view of Stability of supersonic inlets at Mach 1.91 with air injection and suction
Kowalski, K. & Piercy, Thomas G.
June 28, 1956
Primary view of Longitudinal and Lateral Stability Characteristics of a Low-Aspect-Ratio Unswept-Wing Airplane Model at Mach Numbers of 1.82 and 2.01
Spearman, M. Leroy & Driver, Cornelius
January 28, 1956
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