Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests

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090 ⊔ ⊔ ‡aTL500 ‡b.T33 68-00688
100 1 ⊔ ‡aChambers, Joseph R.
245 1 0 ‡aCalculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests / ‡cby Joseph R. Chambers and Sue B. Grafton.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, ‡c1968.
300 ⊔ ⊔ ‡a61 p. : ‡bill. ; ‡c27 cm.
490 0 ⊔ ‡aNASA Technical note ; ‡vNASA TN D-4344
500 ⊔ ⊔ ‡aWork performed at Langley Research Center.
500 ⊔ ⊔ ‡aN68-15941.
504 ⊔ ⊔ ‡aIncludes bibliographical references (p. 19).
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aFlight testing.
650 ⊔ 0 ‡aAirplanes ‡xWings.
650 ⊔ 0 ‡aStability of airplanes, Longitudinal.
650 ⊔ 0 ‡aVertically rising aircraft.
700 1 ⊔ ‡aGrafton, Sue B.
710 2 ⊔ ‡aLangley Research Center.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ⊔ ⊔ ‡a011442905
DAT 0 ⊔ ‡a20101104145037.0 ‡b20141009010000.0
DAT 1 ⊔ ‡a20141112165512.0 ‡b2023-03-14T18:35:02Z
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