Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊

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245 0 0 ‡aRotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊/ ‡cprepared for Langley Research Center.
260 0 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Branch ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1983-
490 0 ‡aNASA contractor report ; ‡v3246
500 ‡aChiefly graphs.
500 ‡a"March 1983"--Cover.
504 ‡aIncludes bibliographical references.
505 1 ‡av. 1. Influence of airplane components for model D / J. N. Ralston.
538 ‡aMode of access: Internet.
650 0 ‡aUnsteady flow (Aerodynamics)
650 0 ‡aSpin (Aerodynamics)
650 0 ‡aWind tunnels ‡xFlow visualization
650 0 ‡aAirplanes ‡xWings
650 0 ‡aRotational motion (Rigid dynamics)
700 1 0 ‡aRalston, J. N.
710 1 0 ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Branch.
710 2 0 ‡aLangley Research Center.
CID ‡a100074504
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DAT 1 ‡a20180312185024.0 ‡b2024-01-20T19:12:26Z
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