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Supersonic Technology Concept Aeroplanes for Environmental Studies
Two-Dimensional Jet Control. Part 2 - a Plane Jet with a Wedge in a Stationary Oblique Flow - Theory
Two-Dimensional Jet Control. Part 1 - a Plane Jet in a Stationary Oblique Flow - Theory
Cart3D Simulations for the First AIAA Sonic Boom Prediction Workshop
Supersonic Business-Jet Concept Designed for Low Sonic Boom
Nitric Acid - Kerosene Rocket Motors: Initial Development Work With Impinging Jet Type Injectors
An Experimental Air-Cushion Vehicle PV-1 Summary Report
Peripheral Jet Air Cushion Vehicle. Energy Study of Hybrid Propulsion, 2
Holographic Flow Visualization (Citations from the NTIS Data Base)
Holographic Flow Visualization (Citations from the NTIS Data Base)
Holographic Flow Visualization. 1968-March, 1980 (Citations from the NTIS Data Base)
Holographic Flow Visualization. 1968-July, 1982 (Citations from the NTIS Data Base)
Holographic Flow Visualization. 1968-June, 1981 (Citations from the NTIS Data Base)
Prediction of Unsteady Separated Transonic Flow Around Missile Configurations
Holographic Flow Visualization (Citations from the NTIS Data Base)
Conceptual Design of a Supersonic Business Jet Propulsion System
Upper-Surface Blowing Nacelle Design Study for a Sweat Wing Airplane at Cruise Conditions
Wind-Tunnel Investigation of a Four-Engine Externally Blowing Jet-Flap STOL Airplane Model
Jet Noise Prediction Comparisons with Scale Model Tests and Learjet Flyover Data
Jet Noise Prediction Comparisons with Scale Model Tests and Learjet Flyover Data
Analytic Calculation of Two-Dimensional Supersonic Jets
Investigation of the Steady Expansion of a Gaseous Axisymmetric Jet into a Vacuum Final Report
CFD Simulation of Liquid Rocket Engine Injectors. Part 1. Simulations of the RCM-1 Experiments
Variation of Pitching Moment with Engine Thrust for a Twin-Engine Commercial Jet Aircraft
Wind Tunnel Model Design for Sonic Boom Studies of Nozzle Jet Flows with Shock Interactions
Peripheral Jet Air Cushion Landing System Spanloader Aircraft. Volume I
Experimental Study of Hypersonic Jets with the Aid of Hot-Wire Anemometer