Lateral stability of an F-100A airplane

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049 ⊔ ⊔ ‡aMAIN
086 0 ⊔ ‡aD 301.45/5:57-563
100 1 ⊔ ‡aGowin, Norman E., ‡eauthor.
245 1 0 ‡aLateral stability of an F-100A airplane / ‡cprepared by Norman E. Gowin.
264 ⊔ 1 ‡aWright Patterson Air Force Base, Ohio : ‡bWright Air Development Center, Air Research and Development Command, United States Air Force, ‡c1957.
300 ⊔ ⊔ ‡a67 pages : ‡billustrations ; ‡c27 cm.
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aWADC technical report ; ‡v57-563
500 ⊔ ⊔ ‡a"Contract No. AF 33(038)-5065"
500 ⊔ ⊔ ‡a"Contract No. AF 33(038)-3384"
500 ⊔ ⊔ ‡a"November 1957."
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aCharts, diagrams, etc.
650 ⊔ 0 ‡aAirplanes ‡xControl.
650 ⊔ 0 ‡aStability of airplanes, Lateral.
650 ⊔ 0 ‡aAirplanes ‡xTail surfaces.
650 ⊔ 0 ‡aAirplanes ‡xWings, Swept-back.
650 ⊔ 0 ‡aAirplanes ‡xModels ‡xTesting.
710 1 ⊔ ‡aUnited States. ‡bAir Force. ‡bAir Research and Development Command. ‡esponsor.
710 2 ⊔ ‡aWright Air Development Center, ‡eissuing body.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
899 ⊔ ⊔ ‡a39015095288976
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