Prediction of axial-flow instabilities in a turbojet engine by use of a multistage compressor simulation on the digital computer

LDR			01355cam a2200325Ia 4500
001			011424904
003			MiAaHDL
005			20141009010000.0
006			m d
007			cr bn ---auaua
008			930325s1975 dcua b f000 0 eng d
035	⊔	⊔	‡asdr-uiuc6360240
035	⊔	⊔	‡a(OCoLC)27801255
040	⊔	⊔	‡aABC ‡cABC ‡dLHL
049	⊔	⊔	‡aUIUU
050	⊔	4	‡aTL521.3.T4 ‡bA3 no. 3134
086	0	⊔	‡aNAS 1.15:X-3134
100	1	⊔	‡aDaniele, Carl J.
245	1	0	‡aPrediction of axial-flow instabilities in a turbojet engine by use of a multistage compressor simulation on the digital computer / ‡cCarl J. Daniele, Ronald J. Blaha, and Kurt Seldner.
260	⊔	⊔	‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1975.
300	⊔	⊔	‡a34 p. : ‡bill. ; ‡c27 cm.
490	0	⊔	‡aNASA technical memorandum ; ‡vNASA TM X-3134
500	⊔	⊔	‡aPrepared at Lewis Research Center.
500	⊔	⊔	‡aCover title.
504	⊔	⊔	‡aIncludes bibliographical references (p. 28).
538	⊔	⊔	‡aMode of access: Internet.
650	⊔	0	‡aAirplanes ‡xTurbojet engines.
650	⊔	0	‡aCompressors ‡xAerodynamics ‡xComputer simulation.
650	⊔	0	‡aAxial flow compressors ‡xComputer simulation.
700	1	⊔	‡aSeldner, Kurt.
700	1	⊔	‡aBlaha, Ronald J.
710	2	⊔	‡aLewis Research Center.
CID	⊔	⊔	‡a011424904
DAT	0	⊔	‡a20101004144356.0 ‡b20141009010000.0
DAT	1	⊔	‡a20141112164151.0 ‡b2024-04-22T18:14:20Z
DAT	2	⊔	‡a2024-04-22T17:30:02Z
CAT	⊔	⊔	‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT	⊔	⊔	‡aBK
HOL	⊔	⊔	‡0sdr-uiuc6360240 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106612762 ‡sUIU ‡16360240
974	⊔	⊔	‡bUIU ‡cUIUC ‡d20240422 ‡sgoogle ‡uuiug.30112106612762 ‡y1975 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018