Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination

LDR 02271cam a2200421Ia 4500
001 100167880
003 MiAaHDL
005 20221205000000.0
006 m d
007 cr bn ---auaua
008 110427e195803 dcua tb f000 0 eng d
035 ⊔ ⊔ ‡a(MiU)990128618370106381
035 ⊔ ⊔ ‡asdr-miu.990128618370106381
035 ⊔ ⊔ ‡z(MiU)MIU01000000000000012861837-goog
035 ⊔ ⊔ ‡a(OCoLC)715348822
035 ⊔ ⊔ ‡z(MiU)Aleph012861837
040 ⊔ ⊔ ‡aLHL ‡cLHL ‡dNACAR
049 ⊔ ⊔ ‡aNACA
086 0 ⊔ ‡aY 3.N 21/5:15/E57K19B
088 ⊔ ⊔ ‡aNACA RM E57K19B
100 1 ⊔ ‡aNettles, J. Cary.
245 1 0 ‡aInvestigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination / ‡cJ. Cary Nettles and Robert C. Campbell.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1958.
300 ⊔ ⊔ ‡a30 p. : ‡bill. ; ‡c27 cm.
490 0 ⊔ ‡aNACA research memorandum ; ‡vE57K19B
500 ⊔ ⊔ ‡aNACA Research Memorandum E57K19B.
500 ⊔ ⊔ ‡a"March 5, 1958."
500 ⊔ ⊔ ‡aTitle from cover.
504 ⊔ ⊔ ‡aIncludes bibliographical references.
520 3 ⊔ ‡aFor a Mach number range from 1.6 to 2.0 and angles of attack from 0 to 9 degrees the occurrence of stall was related to the presence of a pressure deficiency at the hub of the compressor. The referred engine air flow tended to increase as radial distortion level increased. Approaching the inlet buzz limit with the engine operating in or near a stall condition did not affect the minimum stable air flow of the diffuser, and conversely the presence of mild buzz did not affect the compressor stall limit. The stability limits of a 15 degree plus 10 degree double-cone inlet were essentially the same with the engine as with a choked plug.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aCharts, diagrams, etc.
650 ⊔ 0 ‡aCompressors.
650 ⊔ 0 ‡aAerodynamics, Supersonic.
650 ⊔ 0 ‡aVibration (Aeronautics)
650 ⊔ 0 ‡aJet engines ‡xAir intakes.
650 ⊔ 0 ‡aAirplanes ‡xTurbojet engines.
700 1 ⊔ ‡aCampbell, Robert C.
710 2 ⊔ ‡aLewis Flight Propulsion Laboratory.
710 2 ⊔ ‡aUnited States. ‡bNational Adviosry Committee for Aeronautics. ‡tNACA research memorandum.
710 1 ⊔ ‡aUnited States. ‡bNational Advisory Committee for Aeronautics.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
899 ⊔ ⊔ ‡a39015086464131
CID ⊔ ⊔ ‡a100167880
DAT 0 ⊔ ‡b20221205000000.0
DAT 1 ⊔ ‡a20221206110740.0 ‡b2024-04-20T17:42:56Z
CAT ⊔ ⊔ ‡aSDR-MIU ‡cmiu ‡dALMA ‡lprepare.pl-004-008
FMT ⊔ ⊔ ‡aBK
HOL ⊔ ⊔ ‡0sdr-miu.990128618370106381 ‡aMiU ‡bSDR ‡cGWLA ‡f012861837 ‡pmdp.39015086464131 ‡sMIU ‡1990128618370106381
974 ⊔ ⊔ ‡bMIU ‡cGWLA ‡d20240420 ‡sgoogle ‡umdp.39015086464131 ‡y1958 ‡rpd ‡qbib ‡tUS fed doc