Liquefied natural gas as a fuel for supersonic aircraft.
Initial Perturbation Amplitude of Liquid Sheets Produced by Jet-Impingement Nozzles
Study of propellant valve leakage in a vacuum Phase I report, 7 Jun. - 24 Nov. 1965
A Preliminary Investigation of Oxidizer-Rich Oxygen-Hydrogen Combustion Characteristics
Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability
Influence of Ammonia Borane on the Stability of a Liquid Rocket Combustor
NASA's Hydrogen Outpost: The Rocket Systems Area at Plum Brook Station
Conceptual Study on Low-Melting-Point Thermoplastic Fuel/Nitrous Oxide Hybrid Rockoon
A Study of Liquid Propellant Behavior During Periods of Varying Accelerations Final Report
Improved Linearized Breakup Model for the Liquid Sheets Produced by Swirl Atomizers
The effect of surface contamination on contact angles and surface potentials Summary report
Fill Valve Development for the Advanced Liquid Propulsion System (Alps)
Evolvable Cryogenics (eCryo) Project Technology Workshop with Industry: Success Criteria and Wrap-up
Computational Study of Shock-Driven Multiphase Mixing in Scramjet Conditions