Transonic Performance of an Auxiliary Airflow System for Axisymmetric Inlets von Sorensen, Norman E, Latham, Eldon A

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Method for Increasing Wind Tunnel Mach Number for Large-Scale Inlet Testing von Latham, Eldon A, Sorensen, Norman E

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Variable Geometry for Supersonic Mixed-Compression Inlets von Sorensen, Norman E, Latham, Eldon A, Smeltzer, Donald B

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Supersonic inlet contour interpolation von Sorensen, Norman E, Latham, Eldon A

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Advanced supersonic inlet technology von Sorensen, Norman E, Smeltzer, Donald B, Latham, Eldon A

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Investigation of a mixed compression axisymmetric inlet at Mach number 5.3 / by Eldon A. Latham, Norman E. Sorenson and Donald B. Smeltzer von Latham, Eldon A

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Aircraft engine nozzle von SORENSEN, NORMAN E, LATHAM, ELDON A

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Jet engine air intake system von LATHAM, ELDON A, SORENSEN, NORMAN E

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Outboard motor von WILSON ELDON M, POLLOCK LATHAM

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