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acceleration additional aircraft airplane analysis angle of attack Apollo APPENDIX applications approximately cable calculations Center characteristics coefficient computed configuration considered constant crew station defined determine dimension display effects energy engine equation equipment evaluation factor Figure flap flight flow force frequency function given impact included increase indicated intensity limited loss magnetic material measured method mission motor NASA obtained oooooooooo oooooooooo oooooooooo operations performance pilot pitch position presented pressure problem procedures q q q reference Report response ride ring roll rotor shown shows simulated slot solution Space spacecraft stator storage subjects surface task TECHNICAL temperature tion units vibrational winding wires
Page 1 - National Aeronautics and Space Administration Washington, DC 20546 14 Sponsoring Agency Code 17. Key Words (Suggested by Author(s)) 18.
Page 37 - NASA Langley Research Center Hampton, Va. 23665 11. Contract or Grant No. 13. Type of Report and Period Covered 12.
Page 8 - As an aid to the reader, where necessary the original units of measure have been converted to the equivalent value in the Systeme International d
Page 42 - V/STOL tunnel of the wingsurface — jet interaction characteristics of an upper-surface blown model with rectangular exhaust nozzles and a radius flap.
Page 43 - No. 505-02-13-01 11. Contract or Grant No. 12. Sponsoring Agency Name and Address National Aeronautics and Space Administration Washington, DC 20546 13.
Page 48 - The aircraft is suspended from the top of the gantry by two swing cables and is drawn back above the impact surface by a pullback cable. An umbilical cable used for data acquisition is also suspended from the top of the gantry and connects to the top of the aircraft. The test sequence is initiated when the aircraft is released from the pullback cable. The aircraft swings pendulum style into the impact surface. The swing cables are separated from the aircraft by pyrotechnics just prior to impact,...