Tools

LEADER 02555cam a2200529La 4500

001 ocm82514108;

003 OCoLC;

005 20080710132812.0;

007 he bmb024bbca;

008 901031s1989 dcua bb f000 0 eng d;

037 a| N 89-26810b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:4124;

100 1 a| Hallissy, James B.=| ^A784085;

245 10 a| Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /c| James B. Hallissy and Pamela S. Phillips.;

300 a| 225 p. :b| ill. ;c| 28 cm.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 4124;

500 a| "August 1989.";

500 a| "National Aeronautics and Space Administration Cod NTT-4.";

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

504 a| Includes bibliographical references (p. 5-6).;

530 a| Also available via Internet from the NASA Technical Report Server web site. Address as of 7/10/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890017439%5F1989017439.pdf; current access available via PURL.;

650 0 a| Wind tunnels.=| ^A198433;

650 0 a| Airplanesx| Wings.=| ^A39411;

650 0 a| Laminar flow.=| ^A68527;

650 7 a| Aircraft configurations.2| nasat;

650 7 a| Laminar flow.2| nasat;

650 7 a| Pressure distribution.2| nasat;

650 7 a| Variable sweep wings.2| nasat;

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

650 7 a| Wing loading.2| nasat;

700 1 a| Phillips, Pamela S.=| ^A784086;

710 1 a| United States.b| National Aeronautics and Space Administration.b| Scientific and Technical Information Division.=| ^A634451;

830 0 a| NASA technical memorandumv| 4124.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS96586;

949 a| NAS 1.15:4124w| sudoch| joyner32;

596 a| 1;

998 a| 1393348;

999 a| NAS 1.15:4124w| SUDOCc| 1i| MQ2578585d| 8/12/2008l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 8/12/2008x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow / James B. Hallissy and Pamela S. Phillips.

Author/creator	Hallissy, James B.
Other author	Phillips, Pamela S.
Other author	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Format	Microform
Publication Info	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.
Description	225 p. : ill. ; 28 cm.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS96586
Subjects	Wind tunnels. Airplanes--Wings. Laminar flow.

Series	NASA technical memorandum ; 4124 NASA technical memorandum 4124. ^A467613
General note	"August 1989."
General note	"National Aeronautics and Space Administration Cod NTT-4."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 5-6).
Other forms	Also available via Internet from the NASA Technical Report Server web site. Address as of 7/10/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890017439%5F1989017439.pdf; current access available via PURL.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989] 3 microfiches.
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:4124
Stock number	N 89-26810 NASA

Availability

Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:4124	✔ Available

Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow / James B. Hallissy and Pamela S. Phillips.

Click here for more information about this title

Availability