Tools

LEADER 02457cam a2200541Ka 4500

001 ocn166902755;

003 OCoLC;

005 20070905082220.0;

007 he bmb024b|ca;

008 070905s1985 dcu b f000 0 eng d;

037 a| N 86-16199b| NASA;

040 a| GPOc| GPOd| MvI;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:87600;

100 1 a| Johnson, William G.q| (William Garland),d| 1944-=| ^A448593;

245 10 a| Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /c| William G. Johnson, Jr., and Acquilla S. Hill.;

300 a| 1 v.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 87600;

500 a| Prepared at Langley Research Center.;

500 a| GPO Cataloging Record Distribution Program (CRDP).;

530 a| Also available via Internet from the NTRS web site. Address as of 9/04/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860006729%5F1986006729.pdf ; current access is available via PURL.;

650 0 a| Aerofoilsx| Testingv| Statistics.=| ^A333143;

650 0 a| Aerodynamics, Transonic.=| ^A186061;

650 0 a| Reynolds number.=| ^A81900;

650 7 a| Airfoil profiles.2| nasat;

650 7 a| Boeing aircraft.2| nasat;

650 7 a| Cryogenic wind tunnels.2| nasat;

650 7 a| High Reynolds number.2| nasat;

650 7 a| Pressure distribution.2| nasat;

650 7 a| Supercritical airfoils.2| nasat;

650 7 a| Two dimensional bodies.2| nasat;

650 7 a| Wind tunnel models.2| nasat;

650 7 a| Wind tunnel tests.2| nasat;

700 1 a| Hill, Acquilla S.=| ^A448594;

710 2 a| Langley Research Center.=| ^A192893;

830 0 a| NASA technical memorandumv| 87600.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS85654;

949 a| NAS 1.15:87600w| sudoch| joyner32;

596 a| 1;

998 a| 1269398;

999 a| NAS 1.15:87600w| SUDOCc| 1i| MQ2263690l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 10/17/2007x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel / William G. Johnson, Jr., and Acquilla S. Hill.

Author/creator	Johnson, William G., 1944-
Other author	Hill, Acquilla S.
Other author	Langley Research Center.
Format	Microform
Publication Info	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
Description	1 v.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS85654
Subjects	Aerofoils--Testing. --Statistics. Aerodynamics, Transonic. Reynolds number.

Series	NASA technical memorandum ; 87600 NASA technical memorandum 87600. ^A467613
General note	Prepared at Langley Research Center.
General note	GPO Cataloging Record Distribution Program (CRDP).
Other forms	Also available via Internet from the NTRS web site. Address as of 9/04/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860006729%5F1986006729.pdf ; current access is available via PURL.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 3 microfiches.
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:87600
Stock number	N 86-16199 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:87600	✔ Available

Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel / William G. Johnson, Jr., and Acquilla S. Hill.

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