A method for calculating strut and splitter plate noise in exit ducts : theory and verification

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050 ⊔ 4 ‡aTL521.3.C6 ‡bA3 no. 2955
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086 0 ⊔ ‡aNAS 1.26:2955
100 1 ⊔ ‡aFink, Martin R.
245 1 2 ‡aA method for calculating strut and splitter plate noise in exit ducts : ‡btheory and verification / ‡cMartin R. Fink.
260 ⊔ ⊔ ‡aWashington : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Office ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1978.
300 ⊔ ⊔ ‡aiii, 77 p. : ‡bill. ; ‡c27 cm.
490 0 ⊔ ‡aNASA contractor report ; ‡v2955
500 ⊔ ⊔ ‡aIssued Mar. 1978.
500 ⊔ ⊔ ‡aPrepared for Lewis Research Center, under contract NAS3-17863.
504 ⊔ ⊔ ‡aIncludes bibliographical references.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aStruts (Engineering)
650 ⊔ 0 ‡aAirplanes ‡xNoise.
650 ⊔ 0 ‡aAerodynamic noise.
710 2 ⊔ ‡aLewis Research Center.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Office.
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DAT 1 ⊔ ‡a20141112173021.0 ‡b2025-01-01T18:38:25Z
DAT 2 ⊔ ‡a2025-01-01T18:30:02Z
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