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92 items

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Nozzle Control System for a 40 by 40 Inch Supersonic Wind Tunnel
Author(s): Wells, C. B.
Corporate Author(s): ARO, Inc.
Date of Publication: 1963-07
Report number: AEDC TDR 63-129
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Hypersonic Force, Pressure, and Heat Transfer Investigations of Sharp and Blunt Slender Cones
Author(s): Wilkinson, David B., Harrington, Shelby A.
Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Date of Publication: 1963-08
Report number: AEDC TDR 63-177
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Physical and Chemical Properties of Ceramic Bonded Solid Lubricant Films
Author(s): Lavik, Melvin T.;, Medved, Thomas M., Clow, William L.
Corporate Author(s): Midwest Research Institute
Laboratory: Directorate of Materials and Processes
Date of Publication: 1963-01
Report number: WADD TR 60-530 Part IV
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Lubrication Behavior and Chemical Degradation Characteristics of Experimental High Temperature Fluids and Lubricants
Author(s): Hopkins, Vernice, St. John, Andrew D., Wilson, Donnell
Corporate Author(s): Midwest Research Institute
Laboratory: Directorate of Materials and Processes
Date of Publication: 1963-01
Report number: WADD TR 60-855 Part 3
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Theoretical and Experimental Investigation of Arc Plasma-Generation Technology. Part II: Applied Research on Electric Arc Phenomena. Volume 2: Arc Column Theory, Electrode Materials Behavior, and Magnetic Field Arc Discharge Interaction
Author(s): John, R. R., Bade, W. L., Chen, M. M., DeBolt, H., Gibbs, T. W., Hoercher, H., Liebermann, R. W., Neurath, P., Yos, J.
Corporate Author(s): Avco Corporation
Date of Publication: 1963-09
Report number: ASD TDR 62-729 Part 2 Volume 2
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Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps Part I: Mach 5 and 8 Data for Expansion Corner Flows: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 63-679 Part 1
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Pressure Measurement at Mach 19 for a Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Hartofilis, Stavros A.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Division
Date of Publication: 1963-05
Report number: ASD TDR 63-319
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Development of a Low Altitude Turbulence Model for Estimating Gust Loads on Aircraft
Author(s): Lappe, U. O., Thuillier, R. H., Reeves, R. W.
Corporate Author(s): New York University
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-07
Report number: ASD TDR 63-318
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Centrifuge Design Evaluation of the X-20 (Dyna-Soar) Crew Station
Author(s): Snyder, Charles J.
Corporate Author(s): X-20 Engineering Office
Laboratory: X-20 Engineering Office
Date of Publication: 1963-07
Report number: ASD TDR 63-338
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A Study of Selected Contorl-Display Problems for Manned Aerospace Vehicles
Author(s): Pickel, Francis E.
Corporate Author(s): Lear, Inc.
Laboratory: Flight Control Laboratory
Date of Publication: 1963-03
Report number: ASD TDR 63-170

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