Evaluation of a simplified gross thrust calculation technique using two prototype F100 turbofan engines in an altitude facility

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050 ⊔ 4 ‡aTL521.3 ‡b.N18 no. 1482
074 ⊔ ⊔ ‡a830-H-15 (microfiche)
086 0 ⊔ ‡aNAS 1.60:1482
100 1 ⊔ ‡aKurtenbach, Frank J.
245 1 0 ‡aEvaluation of a simplified gross thrust calculation technique using two prototype F100 turbofan engines in an altitude facility / ‡cFrank J. Kurtenbach.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Branch : ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1979.
300 ⊔ ⊔ ‡a27 p. : ‡bill. ; ‡c27 cm.
490 ⊔ 0 ‡aNASA technical paper ; ‡v1482
500 ⊔ ⊔ ‡aSTAR Catetory: 07.
500 ⊔ ⊔ ‡a"June 1979"--Cover.
500 ⊔ ⊔ ‡a"Dryden Flight Research Center."
504 ⊔ ⊔ ‡aIncludes bibliographical references.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aAirplanes ‡xTurbojet engines.
650 ⊔ 0 ‡aAirplanes ‡xMotors ‡xThrust ‡xTesting.
650 ⊔ 0 ‡aAirplanes ‡xMotors ‡xThrust ‡xMathematical models.
710 2 ⊔ ‡aHugh L. Dryden Flight Research Center.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Branch.
CID ⊔ ⊔ ‡a011427198
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DAT 1 ⊔ ‡a20141112173021.0 ‡b2025-01-02T19:04:31Z
DAT 2 ⊔ ‡a2025-01-02T18:30:02Z
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