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A Pressure Data System For A 50-In. Continuous Mach 8 Wind Tunnel
Author(s): Hightower, F. C., Jr.Corporate Author(s): Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-05
Report number: AEDC TDR 62-96
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Source Flow Effects In Conical Hypervelocity Nozzles
Author(s): Whitfield, Jack D., Norfleet, Glenn D.Corporate Author(s): Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-06
Report number: AEDC TDR 62-116
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Compensation Of Dynamic Sting Effects In Hotshot Force Measurements
Author(s): Edenfield, E. E., Ledford, R. L.Corporate Author(s): Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-06
Report number: AEDC TDR 62-122
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Flow Characteristics Of A 40-Inch Wind Tunnel At Mach Numbers 1.5 To 6
Author(s): Coats, Jack D.Corporate Author(s): Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-06
Report number: AEDC TDR 62-130
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Inductive Power Supply For A Hotshot-Type Tunnel
Author(s): Fillers, A. H., Jr.Corporate Author(s): Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-07
Report number: AEDC TDR 62-137
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Radio Telemetry of Stagnation Pressure from a wind Tunnel Model Magnetically Supported in Supersonic Flow,
Author(s): Clemens, P. L.Corporate Author(s): Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-07
Report number: AEDC TDR 62-141
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