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74 items

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Mollier Diagram for Air
Author(s): Little, Wanda J.
Corporate Author(s): ARO, Inc.
Date of Publication: 1963-09
Report number: AEDC TDR 63-190
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A Technique for Measuring a Local Gas Density Using Scattered Gamma Radiation
Author(s): Shepard, J. E., Dicks, J. B.
Corporate Author(s): ARO, Inc.
Date of Publication: 1963-11
Report number: AEDC TDR 63-187
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Boundary-Layer Characteristics at Mac Numbers 2 through 5 in the Test Section of the 12-Inch Supersonic Tunnel
Author(s): Bell. D. R.
Corporate Author(s): ARO, Inc.
Date of Publication: 1963-09
Report number: AEDC TDR 63-192
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Pressures in the Stagnation Regions of Blunt Bodies in the Viscous-Layer to Merged-Layer Regimes of Rarefied Flow
Author(s): Potter, J. Leith, Bailey, Allan B.
Corporate Author(s): ARO, Inc.
Date of Publication: 1963-09
Report number: AEDC TDR 63-168
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Pressure Distribution and Flow Visualization Tests of a 1.5 Elliptic Cone at Mach 10
Author(s): Palko, R. L., Ray, A. D.
Corporate Author(s): ARO, Inc.
Date of Publication: 1963-08
Report number: AEDC TDR 63-163
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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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An Aerodynamic Coefficient Prediction Technique for Slender Bodies with Low Aspect Ratio Fins at Mach Numbers from 0.6 to 3.0 and Angles of Attack from 0 to 180 Degrees
Author(s): Baker, William B., Jr.
Corporate Author(s): ARO, Inc.
Laboratory: Propulsion and Wind Tunnel Facility
Date of Publication: 1978-03
Report number: AEDC TR 77-97

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