Investigation of flying qualities of military aircraft at high angles of attack. Volume I, Technical results

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049 ⊔ ⊔ ‡aMAIN
086 0 ⊔ ‡aD 301.45/46-2:74-61 Volume I
100 1 ⊔ ‡aJohnston, Donald E., ‡eauthor.
245 1 0 ‡aInvestigation of flying qualities of military aircraft at high angles of attack. ‡nVolume I, ‡pTechnical results / ‡cby Donald E. Johnson, Irving L. Ashkenas, Jeffrey R. Hogge.
264 ⊔ 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Systems Command, ‡c1974.
300 ⊔ ⊔ ‡axv, 143 pages : ‡billustrations ; ‡c28 cm.
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aAir Force Flight Dynamics Laboratory (U.S.). Technical report ; ‡vAFFDL TR 74-61 Volume I
500 ⊔ ⊔ ‡a"June 1974."
504 ⊔ ⊔ ‡aIncludes bibliograpic references (pages 141-143)
520 ⊔ ⊔ ‡aAttention has been focused on departure (e.g., nose slice, wing rock) and recovery of military aircraft as opposed to spin entry. The approach has been to analytically identify and validate key flying quality parameters, to qualitatively assess and verify these through piloted simulation, and to measure and quantify effects on key dynamic parameters of pilot describing functions.
536 ⊔ ⊔ ‡aReport prepared by Systems Technology, Inc., Hawthorne, California, under contract no. ‡bF33615-73-C-3101.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aAirplanes, Military.
650 ⊔ 0 ‡aStalling (Aerodynamics)
650 ⊔ 0 ‡aSpin (Aerodynamics)
650 ⊔ 0 ‡aAngle of attack (Aerodynamics)
700 1 ⊔ ‡aHogge, Jeffrey R., ‡eauthor.
700 1 ⊔ ‡aAshkenas, Irving L., ‡eauthor.
710 2 ⊔ ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor.
710 2 ⊔ ‡aSystems Technology, Inc., ‡esponsor.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
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