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90 items
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An Experimental Study of Diffusers in an Open-Jet, Low-Density, Hypersonic Wind Tunnel
Author(s): Boylan, David E.Corporate Author(s): ARO, Inc.
Date of Publication: 1964-04
Report number: AEDC TDR 64-47
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Charts of Normal Shock Wave Properties in Imperfect Air
Author(s): Lewis, Clark H., Burgess, E. G., IIICorporate Author(s): ARO, Inc.
Date of Publication: 1964-03
Report number: AEDC TDR 64-43
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Specific Heat and Speed of Sound Data for Imperfect Air
Author(s): Lewis, Clark H., Neel, Charles A.Corporate Author(s): ARO, Inc.
Date of Publication: 1964-04
Report number: AEDC TDR 64-36
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Condensation in Hotshot Tunnels
Author(s): Griffith, B. J., Deskins, H. E., Little, H. R.Corporate Author(s): ARO, Inc.
Date of Publication: 1964-02
Report number: AEDC TDR 64-35
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Force and Pressure Tests of an Agard Calibration Model B at a Mach Number of 10
Author(s): Matthews, R. K., Trimmer, L. L.Corporate Author(s): ARO, Inc.
Date of Publication: 1964-02
Report number: AEDC TDR 64-31
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Heat-Transfer and Shadowgraph Tests of Several Elliptical Lifting Bodies at Mach 10
Author(s): Hillsamer, M. E., Rhudy, J. P.Corporate Author(s): ARO, Inc.
Date of Publication: 1964-02
Report number: AEDC TDR 64-19
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Investigation of Flow Separation on a Two-Dimensional Flat Plate Having a Variable-Span Trailing-Edge Flap at M = 3 and 5
Author(s): Pate, S. R.Corporate Author(s): ARO, Inc.
Date of Publication: 1964-03
Report number: AEDC TDR 64-14
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Comparison of Hotshot Tunnel Force, Pressure, Heat-Transfer and Shock Shape Data with Shock Tunnel Data
Author(s): Edenfield, E. E.Corporate Author(s): ARO, Inc.
Date of Publication: 1964-01
Report number: AEDC TDR 64-1
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Altimeter Display Study Part I. Summary and Review of Data Requirements
Author(s): Matheny, W. G.Corporate Author(s): Bell Helicopter Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: ASD TDR 63-621 Part 1
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Altimeter Display Study Part II. Handbook for Static Testing of Altimeters
Author(s): Elam, C. B., Matheny, W. G., Schum, D. A.Corporate Author(s): Bell Helicopter Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: ASD TDR 63-622 Part 2
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