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ADMINISTRATION AERONAUTICS AND SPACE analysis angle APPENDIX approach Atmosphere AVSSE bending calculated Center coating coefficient compressible computed considered constant Continued cylinder derivatives determined differences direction distribution dynamic edge effects energy engine equation errors Experiment face factor film thickness flight flow fluid force frequencies friction function given heating important increase indicated input leakage limited linear load longitudinal lubrication mass material measurement Mechanical Impact Test mode motion NASA nonlinear normal obtained occurred operation oxygen panel parameter percent performance presented pressure propellant properties ratio reference response rotor Sample seal shear shown in figure shows soundings Space stress structural surface TABLE TECHNICAL Teflon temperature thermal thickness tile turbulent Unit values variables velocity washout wind
Page 61 - Hence a particle of fluid, at each stage of its progress along the tapering contraction, is passing from a region of higher pressure to a region of lower pressure...
Page 22 - Deveikis, William D.; and Hunt, L. Roane: Loading and Heating of a Large Flat Plate at Mach 7 in the Langley 8-Foot High-Temperature Structures Tunnel.
Page 97 - NASA Langley Research Center Hampton, Va. 23665 11. Contract or Grant No.
Page 94 - Throughflow in Concentric and Eccentric Annuli of Fine Clearance With and Without Relative Motion of the Boundaries,
Page 65 - Nihart, GJ; and Smith, CP: Compatibility of Materials With 7500 PSI Oxygen.
Page 38 - An Actuator Extension Transformation for a Motion Simulator and an Inverse Transformation Applying Newton-Raphson's Method.
Page 3 - For sale by the National Technical Information Service. Springfield, Virginia 22161 1 Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA CR-2885 4. Title and Subtitle 5. Report Date "Computers for Real Time Market Survey" Flight Simulation: A July 1977 6.