The performance of conical supersonic scoop inlets on circular fuselages

LDR 01194nam a2200301Ka 4500
001 100168008
003 MiAaHDL
005 20221205000000.0
006 m d
007 cr bn ---auaua
008 121113s1953 dcua b f000 0 eng d
035 ‡a(MiU)990128619620106381
035 ‡asdr-miu.990128619620106381
035 ‡z(MiU)MIU01000000000000012861962-goog
035 ‡a(OCoLC)817733247
035 ‡z(MiU)Aleph012861962
040 ‡aNACAR ‡cNACAR
049 ‡aNACA
086 0 ‡aY 3.N21/5:15/L53I14a
100 1 ‡aHasel, Lowell E.
245 1 4 ‡aThe performance of conical supersonic scoop inlets on circular fuselages / ‡cBy Lowell E. Hasel.
260 ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1953.
300 ‡a12 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNational Advisory Committee for Aeronautics research memorandum ; ‡vL53I14a
500 ‡a"November 17, 1953."
504 ‡aIncludes bibliographical references (p. 7).
538 ‡aMode of access: Internet.
650 0 ‡aAirplanes ‡xAir ducts.
650 0 ‡aAirplanes ‡xFuselage.
710 2 ‡aLangley Aeronautical Laboratory.
710 2 ‡aUnited States. ‡bNational Adviosry Committee for Aeronautics. ‡tNACA research memorandum.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015086465427
CID ‡a100168008
DAT 0 ‡b20221205000000.0
DAT 1 ‡a20221207140737.0 ‡b2024-03-16T17:39:38Z
CAT ‡aSDR-MIU ‡cmiu ‡dALMA ‡lprepare.pl-004-008
FMT ‡aBK
HOL ‡0sdr-miu.990128619620106381 ‡aMiU ‡bSDR ‡cGWLA ‡f012861962 ‡pmdp.39015086465427 ‡sMIU ‡1990128619620106381
974 ‡bMIU ‡cGWLA ‡d20240316 ‡sgoogle ‡umdp.39015086465427 ‡y1953 ‡rpd ‡qbib ‡tUS fed doc