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A Study of the Influence of Lubricants on High-Speed Rolling-Contact Bearing Performance: Part V. Research on Elastohydrodynamic Lubrication on High-Speed Rolling Contacts
Author(s): Kannel, Jerrold, Walowit, J. A., Bell, J. Clarence
Corporate Author(s): Battelle Memorial Institute
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1965-07
Report number: ASD TDR 61-643 Part 5
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A Conical Thin-Shock-Layer Theory Uniformly Valid in the Entropy Layer
Author(s): Melnik, Robert E.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-01
Report number: FDL TDR 64-82
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Pressure Measurements at Mach 8 on an Aerodynamically Controllable Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Meckler, Lawrence
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1965-06
Report number: FDL TDR 64-124
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Theory Of Stage II Fatigue Crack Propagation
Author(s): Grosskreutz, J. C.
Corporate Author(s): Midwest Research Inst Kansas City MO
Laboratory: AF Materials Laboratory
Date of Publication: 1965-03
Report number: AFML TR 64-415
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Ultrasonic Wave Propagation And Interaction In Solid Materials
Author(s): Rollins, F. R., Jr.
Corporate Author(s): Midwest Research Institute, Kansas City, MO
Date of Publication: 1965-04
Report number: ML TDR 64-21 Part 2
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Thermal Protection Systems. Application Research Of Materials Properties And Structural Concepts
Author(s): Hurwicz, Henryk, Mascola, Robert
Corporate Author(s): Avco Corp Wilmington Mass Research And Advanced Development Div
Laboratory: AF Materials Laboratory
Date of Publication: 1965-01
Report number: ML TDR 64-82
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Research on Gas Lubrication at High Temperatures and Low Flow Rates
Author(s): Lewis, P., Eusepi, M.
Corporate Author(s): Mechanical Technology, Inc.
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1965-03
Report number: APL TDR 64-56 Part 2
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Nonlinear Thermoelasitc Effects on Hypersonic Stability and Control, Part III: Simulation, Measurement and Analysis of Nonlinear Static Aerothermoelastic Behavior of a 45 Degree Delta Wing
Author(s): Batt, James R.
Corporate Author(s): Bell Aerosystems Co.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-02
Report number: FDL TDR 64-16 Part 3
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Transient Dynamic Response of Orbiting Space Stations
Author(s): Tai, C. L., Andrew, L. V., Loh, M. M. H., Kamrath, P. C.
Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-02
Report number: FDL TDR 64-25
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Investigation Of Propellant Actuated Devices For Use In Emergency Crew Escape Systems For Advanced Aerospace Vehicles. Phase III. Design Study.
Author(s): Bleikamp, R. H., Lake, E. R., McGovern, D. R.
Corporate Author(s): McDonnell Aircraft Corp St Louis MO
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-04
Report number: AFFDL TR 65-26 Part 2

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