Performance of external-internal compression inlet with abrupt internal turning at Mach numbers 3.0 to 2.0
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Obery, Leonard J↗
Engineering topics
Stitt, Leonard E
Publications and source records attributed to Stitt, Leonard E.
An inlet design concept to reduce flow distortion at angle of attack
Flow distortions were measured at the inlet face and diffuser exit of three axisymmetric inlets operating at angles of attack of 0 degree to 14 degrees and at a Mach number of 1.91.
Schueller, Carl F↗
Performance of several half-conical side inlets at supersonic and subsonic speeds
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Stitt, Leonard E↗
Effect of throat bleed on the supersonic performance of a half-conical side-inlet system
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Stitt, Leonard E↗
Effect on Ejector Performance of Varying Diameter Ratio by Simulated Iris Flaps
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Valerino, Alfred S↗
Effect of free-stream Mach number on gross-force and pumping characteristics of several ejectors
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Stitt, Leonard E↗
Investigation of Several Double-ramp Side Inlets
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Stitt, Leonard E↗
Evaluation at Supersonic Speeds of Twin-duct Side-intake System with Two-dimensional Double-shock Inlets
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Obery, Leonard J↗
Investigation at Mach Numbers 1.5 and 1.7 of Twin-duct Side Air-intake System with 9 Degree Compression Ramp Including Modifications to Boundary-layer-removal Wedges and Effects of a Bypass System
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Obery, Leonard J↗