000237317 000__ 02647cam\a2200553Ka\45e0
000237317 001__ 237317
000237317 005__ 20220217104408.0
000237317 008__ 000717m19999999vau\\\\\b\\\\f100\0\eng\d
000237317 035__ $$a(OCoLC)ocm44596209
000237317 035__ $$a237317
000237317 037__ $$a20000014369 thru 20000014384 (v.1, pt.1)$$bNASA
000237317 037__ $$a20000020876 thru 20000020887 (v.1, pt.2)$$bNASA
000237317 037__ $$a20000024815 thru 20000024823 (v.2, pt.1)$$bNASA
000237317 037__ $$a20000021080 thru 20000021088 (v.2, pt.2)$$bNASA
000237317 040__ $$aGPO$$cGPO
000237317 049__ $$aISEA
000237317 074__ $$a0830-H-10 (MF)
000237317 0860_ $$aNAS 1.55:209704/V.1/PT.1-
000237317 1112_ $$aNASA High-Speed Research Program Aerodynamic Performance Workshop$$d(1999 :$$cAnaheim, Calif.)
000237317 24510 $$a1999 NASA High-Speed Research Program Aerodynamic Performance Workshop$$h[microform] :$$bproceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington D.C., and held in Anaheim, California, February 8-12, 1999 /$$cedited by David E. Hahne.
000237317 2462_ $$a1999 NASA High Speed Research Program Aerodynamic Performance Workshop
000237317 2463_ $$aNASA High Speed Research Program Aerodynamic Performance Workshop
000237317 260__ $$aHampton, Va. :$$bNational Aeronautics and Space Administration, Langley Research Center ;$$a[Springfield, Va. :$$bNational Technical Information Service, distributor,$$c1999- ]
000237317 300__ $$av.
000237317 4901_ $$aNASA/CP ;$$v1999-209704/VOL1/PT1-PT2, VOL2/PT1-PT2
000237317 500__ $$aShipping list no.: 2000-0697-M (v.1, pts.1-2, v.2, pt.1), 2000-0908-M (v.2, pt.2).
000237317 5051_ $$av. 1. Configuration aerodynamics -- v. 2. High lift.
000237317 533__ $$aMicrofiche.$$b[Washington, D.C. :$$cNational Aeronautics and Space Administration,$$d2000- ]$$e<29> microfiches.
000237317 650_7 $$aAerodynamic characteristics.$$2nasat
000237317 650_7 $$aAerodynamic configurations.$$2nasat
000237317 650_7 $$aAerodynamic stability.$$2nasat
000237317 650_7 $$aAircraft design.$$2nasat
000237317 650_7 $$aBody-wing configurations.$$2nasat
000237317 650_7 $$aCanard configurations.$$2nasat
000237317 650_7 $$aCivil aviation.$$2nasat
000237317 650_7 $$aComputational fluid dynamics.$$2nasat
000237317 650_7 $$aEngine airframe integration.$$2nasat
000237317 650_7 $$aOptimization.$$2nasat
000237317 650_7 $$aPerformance prediction.$$2nasat
000237317 650_7 $$aSupersonic transports.$$2nasat
000237317 650_7 $$aWing nacelle configurations.$$2nasat
000237317 650_7 $$aWind tunnel tests.$$2nasat
000237317 7001_ $$aHahne, David E.
000237317 7101_ $$aUnited States.$$bNational Aeronautics and Space Administration.
000237317 7102_ $$aLangley Research Center.
000237317 74002 $$aConfiguration aerodynamics.
000237317 74002 $$aHigh lift.
000237317 830_0 $$aNASA conference publication ;$$v209704.
000237317 85230 $$bdfich$$hNAS 1.55:$$i209704/
000237317 86631 $$avol.1/pt.1
000237317 86631 $$avol.1/pt.2
000237317 86631 $$avol.2/pt.1
000237317 86631 $$avol.2/pt.2
000237317 909CO $$ooai:library.usi.edu:237317$$pGLOBAL_SET
000237317 980__ $$aBIB
000237317 980__ $$aGOV RESOURCE
000237317 994__ $$aE0$$bISE