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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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Deep-stall characteristics of T-tailed aircraft configurations and recovery procedures, noting parameters of pitch-up, angle of attack, etc
Flight tests were made of the flying qualities of an F-47D-30 airplane to determine the longitudinal stability and control and stalling characteristics.
Simulator studies of aircraft deep-stall problem - pitch control problem
Wind tunnel determination of factors contributing to post-stall longitudinal stability of t-tail transport configurations
Fixed base simulation study of T-tail aircraft deep stall and recovery
Wind tunnel research of deep stall aerodynamic characteristics of T tail analyzed as preliminary design guide
T tail aircraft in deep stall conditions in fixed- base cockpit simulation at large angle of attack
Performance and stall limits of YTF30-P-1 turbofan engine with uniform compressor inlet flow
Steady state and dynamic distortion influence on performance and stall of turbofan engine, discussing compressor instrumentation, tests and simulation data
Performance and stall limits of afterburner-type turbofan engine with and without inlet flow distortion
Inlet pressure fluctuation in XB-70 aircraft during takeoff and prior to compressor stall at Mach 2.5
Dynamic airfoil stall simulation in wind tunnels, considering pitch rate, Reynolds number, oscillation and test equipment effects
Experimental data and performance of honeycomb rotor shroud configuration to improve stall margin of 0.5 hub tip ratio single stage compressor
Flow distribution data for solid and honeycomb rotor shrouds to improve stall margin of 0.5 hub tip ratio single stage compressor
Effects of turbojet engine unstart on engine operation and characteristics of stall propagation through compressor and inlet system
Effects of engine inlet disturbances on engine stall performance
Feasibility of using fixed simulator to determine stall and spin characteristics of fighter aircraft
Effect of circumferential, radial, and combined pressure distortions on stall margin of J-85 engine