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Optical Measurement Techniques for Rocket Engine Testing and Component Applications
NASA Acoustic Stirling IRAD: Thermal Recovery Energy Conversion in Aircraft
Comparison of Three Thrust Calculation Methods Using in-Flight Thrust Data
Materials Selection for Task 13 Hot-Bleed Radiation-Cooled Skirt Application, Nerva
Aircraft Performance Optimization with Thrust Vector Control
Waking a Giant: Bringing the Saturn F-1 Engine Back to Life
Overview of CMC Research at NASA Glenn Research Center
Noise from Aft Deck Exhaust Nozzles: Differences in Experimental Embodiments
Data Base for the Prediction of Airframe/Propulsion System Interference Effects
Black Brant Rocket Aaf-4-17 Launched at Churchill Research Range, 19 January 1969
Ejector Effects on a Supersonic Nozzle at Low Altitude and Mach Number
Aeroacoustics of Propulsion Airframe Integration: Overview of NASA's Research
Internal Aerodynamics Manual. Volume I
Flight Investigation of Installation Effects on a Plug Nozzle Installed on an Underwing Nacelle
Pneumatic Instrumentation Lines and Their Use in Measuring Rocket Nozzle Pressure
LARVE, a Hypersonic Flight Test Facility Launched by Ariane 4
Powering Characteristics of an Lcvp with Open Screw and Kort Nozzles from Tests with Model 4031-1
Method of Calculating Rocket Engine Nozzle Contour for Optimum Thrust
Comparison of the Ohio State University and Penn State University Skid System Water Nozzle
An Experimental Investigation of the Dual Chamber Rocket
Status Report of the Hypersonic Facility of the Polytechnic Institute of Brooklyn
Fabrication of Composite Combustion Chamber/Nozzle for Fastrac Engine
Investigation of the Rocket Induced Flow Field in a Rectangular Duct
Computational Analysis of Apollo Capsule Testing in HIEST Facility