Effect of structural flexibility on the design of vibration-isolating mounts for aircraft engines

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035 ⊔ ⊔ ‡asdr-uiuc6368970
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040 ⊔ ⊔ ‡aGPO ‡cGPO ‡dABC
049 ⊔ ⊔ ‡aUIUU
050 ⊔ 4 ‡aTL521.3.T4 ‡bA3 no. 85725
074 ⊔ ⊔ ‡a830-D (microfiche)
086 0 ⊔ ‡aNAS 1.15:85725
100 1 ⊔ ‡aPhillips, William H.
245 1 0 ‡aEffect of structural flexibility on the design of vibration-isolating mounts for aircraft engines / ‡cWilliam H. Phillips.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Office ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1984.
300 ⊔ ⊔ ‡a21 p. : ‡bill. ; ‡c28 cm.
490 ⊔ 0 ‡aNASA technical memorandum ; ‡v85725
500 ⊔ ⊔ ‡aSubject category 39.
500 ⊔ ⊔ ‡a"February 1984"--Cover.
500 ⊔ ⊔ ‡aDistributed to depository libraries in microfiche.
504 ⊔ ⊔ ‡aIncludes bibliographical references.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aAirplanes ‡xMotors ‡xDesign and construction.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Office.
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DAT 1 ⊔ ‡a20141112173021.0 ‡b2025-01-01T19:17:53Z
DAT 2 ⊔ ‡a2025-01-01T18:30:02Z
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