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Experience With An Overexpanded Nozzle In A Low-Density, Hypervelocity Wind Tunnel
Author(s): Potter, J. Leith, Boylan, David E.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-04
Report number: AEDC TDR 62-85
full text available
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
full text available
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
full text available
Experimental Heat Transfer to Blunt Axisymmetric Bodies Near the Limit of Continuum Flow
Author(s): Potter, J. Leith, Miller, John T.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-08
Report number: AEDC TDR 62-155
full text available
Fatigue Tests and Crack Detection on Some Types of Axial-Flow Compressor Rotor Blades
Author(s): Thomas, R. E.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-10
Report number: AEDC TDR 62-168
full text available
Tables of the Thermodynamic Properties of Nitrogen From 100 to 1500°K
Author(s): Little, Wanda J., Neel, C. A.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-09
Report number: AEDC TDR 62-170
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- Bailey, A. B. (2)
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