Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles

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050 ⊔ 4 ‡aTL521.3 ‡b.N18 no. 1771
074 ⊔ ⊔ ‡a830-H-15 (microfiche)
086 0 ⊔ ‡aNAS 1.60:1771
100 1 ⊔ ‡aYetter, Jeffery A.
245 1 0 ‡aEffects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles / ‡cJeffery A. Yetter, Laurance D. Leavitt.
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], ‡c1980.
300 ⊔ ⊔ ‡a116 p. : ‡bill ; ‡c27 cm.
490 ⊔ 0 ‡aNASA technical paper ; ‡v1771
500 ⊔ ⊔ ‡aDec. 1980.
500 ⊔ ⊔ ‡a"Langley Research Center."
500 ⊔ ⊔ ‡a"Joint Institute for Advancement of Flight Sciences."
504 ⊔ ⊔ ‡aIncludes bibliographical references.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aJet engines.
650 ⊔ 0 ‡aAerodynames.
650 ⊔ 0 ‡aExhaust nozzles.
700 1 ⊔ ‡aLeavitt, Laurence D.
710 2 ⊔ ‡aLangley Research Center.
710 2 ⊔ ‡aJoint Institute for Advancement of Flight Sciences.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Branch.
CID ⊔ ⊔ ‡a011427812
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DAT 1 ⊔ ‡a20141112173021.0 ‡b2025-01-01T19:18:07Z
DAT 2 ⊔ ‡a2025-01-01T18:30:02Z
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