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Equations and Charts for the Evaluation of the Hypersonic Aerodynamic Characteristics of Lifting Configurations by the Newtonian Theory
Author(s): Clark, E. L., Trimmer, L. L.
Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1964-03
Report number: AEDC TDR 64-25
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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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Theoretical Base Pressure Analysis of Axisymmetric Ejectors Without Induced Flow
Author(s): Bauer, R. C.
Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1964-01
Report number: AEDC TDR 64-3
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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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Development of a Computer Program for the Analysis of One-Dimensional Magnetohydrodynamic Flow Problems
Author(s): Wilson, D. R., Clouse, C. E., Schaetzle, W. J.
Corporate Author(s): ARO, Inc.
Date of Publication: 1964-01
Report number: AEDC TDR 63-215
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Missile Motion Sensitivity to Dynamic Stability Derivatives
Author(s): Langham, T. F.
Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1980-09-01
Report number: AEDC TR 80-11
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A Description of a Forced-Oscillation Test Mechanism for Measuring Dynamic-Stability Derivatives in Roll
Author(s): Burt, G. E.
Corporate Author(s): ARO, Inc.
Laboratory: Von Karman Gas Dynamics Facility
Date of Publication: 1973-06
Report number: AEDC TR 73-49
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Analytical Study of Ventilated Wind Tunnel Boundary Interference on V/STOL Models Including Wake Curvature and Decay Effects
Author(s): Kraft, E. M.
Corporate Author(s): ARO, Inc.
Laboratory: Propulsion Wind Tunnel Facility
Date of Publication: 1974-11
Report number: AEDC TR 74-51
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An Investigation of Separated Flow About a Hemisphere-Cylinder at 0- to 19-Deg Incidence in the Mach Number Range from 0.6 to 1.5
Author(s): Hsieh, T.
Corporate Author(s): ARO, Inc.
Laboratory: Propulsion and Wind Tunnel Facility
Date of Publication: 1976-11
Report number: AEDC TR 76-112

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