Rotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 8⁰ to 90⁰

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074 ‡a830-H-14 (microfiche)
086 0 ‡aNAS 1.26:3516
100 1 0 ‡aBarnhart, Billy.
245 1 0 ‡aRotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 8⁰ to 90⁰ / ‡cBilly Barnhart ; prepared for Langley Research Center under contract NAS1-16205.
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], ‡c1982.
490 0 ‡aNASA contractor report ; ‡v3516
500 ‡aSubject Category 02.
500 ‡a"May 1982"--Cover.
504 ‡aIncludes bibliographical references.
538 ‡aMode of access: Internet.
650 0 ‡aSpin (Aerodynamics)
650 0 ‡aWind tunnels
650 0 ‡aEagle (Jet fighter plane) ‡xTesting.
710 1 0 ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Branch.
710 2 0 ‡aLangley Research Center.
CID ‡a100074420
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DAT 1 ‡a20180312185024.0 ‡b2023-10-04T17:55:53Z
DAT 2 ‡a2023-10-04T17:30:02Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lprepare.pl-004-007
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