NASA technical note

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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 5 - COMPARISON OF A LINEAR AND A NONLINEAR WASHOUT FOR MOTION SIMULATORS UTILIZING OBJECTIVE AND SUBJECTIVE DATA FROM CTOL TRANSPORT LANDING APPROACHES Russell V Parrish and Dennis J Martin.
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.
Page 41 - N (Ib) 400 341 (90 000) Center of gravity 0.31c Flap deflection, deg 40 Landing gear Down Damping ratio for Short period 0.562 Long period 0.089 Dutch roll 0.039 Period, sec, for Short period 6.30 Long period 44.3 Dutch roll 5.12 TABLE...

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