Method for obtaining aerodynamic data on hypersonic configurations with scramjet exhaust flow simulation

LDR 01567cam a2200349Ii 4500
001 011430737
003 MiAaHDL
005 20141009010000.0
006 m d
007 cr bn ---auaua
008 780513s1977 dcua b f000 0 eng d
035 ⊔ ⊔ ‡asdr-uiuc6384651
035 ⊔ ⊔ ‡a(OCoLC)3891537
037 ⊔ ⊔ ‡b22161
040 ⊔ ⊔ ‡aGPO ‡cGPO ‡dABC ‡dOCLCQ
049 ⊔ ⊔ ‡aUIUU
050 ⊔ 4 ‡aTL521.3.C6 ‡bA3 no. 2831
086 0 ⊔ ‡aNAS 1.26:2831
100 1 ⊔ ‡aHartill, William R.
245 1 0 ‡aMethod for obtaining aerodynamic data on hypersonic configurations with scramjet exhaust flow simulation / ‡cWilliam R. Hartill.
260 ⊔ ⊔ ‡aWashington : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1977.
300 ⊔ ⊔ ‡aiv, 74 p. : ‡bill. ; ‡c27 cm.
490 0 ⊔ ‡aNASA contractor report ; ‡vNASA CR-2831
500 ⊔ ⊔ ‡aIssued June 1977.
500 ⊔ ⊔ ‡aPrepared by Rockwell International Corporation, Los Angeles Aircraft Division, under contract no. NAS1-14320.
504 ⊔ ⊔ ‡aIncludes bibliographical references.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aHypersonic wind tunnels ‡xEquipment and supplies.
650 ⊔ 0 ‡aJets ‡xFluid dynamics.
650 ⊔ 0 ‡aAirplanes ‡xRamjet engines ‡xCombustion.
650 ⊔ 0 ‡aAirplanes ‡xScramjet engines.
650 ⊔ 0 ‡aAerodynamics, Hypersonic.
650 ⊔ 0 ‡aHypersonic planes ‡xModels ‡xTesting.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ⊔ ⊔ ‡a011430737
DAT 0 ⊔ ‡a20101026101447.0 ‡b20141009010000.0
DAT 1 ⊔ ‡a20141112164151.0 ‡b2025-01-02T19:05:23Z
DAT 2 ⊔ ‡a2025-01-02T18:30:02Z
CAT ⊔ ⊔ ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ⊔ ⊔ ‡aBK
HOL ⊔ ⊔ ‡0sdr-uiuc6384651 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106734939 ‡sUIU ‡16384651
974 ⊔ ⊔ ‡bUIU ‡cUIUC ‡d20250102 ‡sgoogle ‡uuiug.30112106734939 ‡y1977 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2019