Advanced Propulsion System Studies for General Aviation Aircraft
New Potentials for Conventional Aircraft when Powered by Hydrogen-Enriched Gasoline
Producing Holograms of Reacting Sprays in Liquid Propellant Rocket Engines Final Report
The Calibration of a Deutz F8L413 Diesel and Development of an On-Board BHP-Indicator
Space Shuttle Orbital Maneuvering Engine Platelet Injector Program
Hydrogen-Oxygen Auxiliary Propulsion for the Space Shuttle. Volume 1 High Pressure Thrusters
Development of a Short-Length Turbojet Combustor Summary Report, 3 Jun. 1965 - 18 Apr. 1967
Advanced Methods for Aircraft Engine Thrust and Noise Benefits: Nozzle-Inlet Flow Analysis
Development of Liquid Oxygen/Liquid Hydrogen Thrust Chamber for the M-1 Engine
Atomization of Impinging Liquid Jets in a Supersonic Crossflow
Lightweight Two-Stroke Cycle Aircraft Diesel Engine Technology Enablement Program. Volume 2
Lightweight Two-Stroke Cycle Aircraft Diesel Engine Technology Enablement Program. Volume 3