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001 on1419919977;

003 OCoLC;

005 20250120152051.0;

006 m o d f ;

007 cr b|||||||abp;

007 cr b|||||||ada;

008 240203s1959 dcua obt f000 0 eng c;

019 a| 761386446;

035 a| (Sirsi) o1419919977;

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:X-47;

100 1 a| Driver, Cornelius,0| https://id.loc.gov/authorities/names/no2007061267,e| author.=| ^A1438444;

245 10 a| Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 /c| by Cornelius Driver and M. Leroy Spearman.;

264 1 a| Washington :b| National Aeronautics and Space Administration,c| September 1959.;

300 a| 1 online resource (28 pages) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| X-47;

500 a| "September 1959.";

500 a| In scope of the U.S. Government Publishing Office Cataloging and Indexing Program (C&I) and Federal Depository Library Program (FDLP).;

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

504 a| Includes bibliographical references (page 8).;

588 a| Description based on online resource; title from PDF title page (NASA, viewed Nov. 25, 2024).;

650 7 a| Mach number.2| nasat;

650 0 a| Stability of airplanes.0| https://id.loc.gov/authorities/subjects/sh85127186=| ^A313010;

650 0 a| Airplanesx| Tail surfaces.0| https://id.loc.gov/authorities/subjects/sh85002903=| ^A687177;

650 0 a| Aerodynamics, Supersonic.0| https://id.loc.gov/authorities/subjects/sh85001297=| ^A47290;

650 7 a| Aerodynamics, Supersonic.2| fast0| (OCoLC)fst00798221;

650 7 a| Airplanesx| Tail surfaces.2| fast0| (OCoLC)fst00803481;

650 7 a| Stability of airplanes.2| fast0| (OCoLC)fst01131210;

700 1 a| Spearman, M. Leroy,0| https://id.loc.gov/authorities/names/n84213710,e| author.=| ^A441239;

830 0 a| NASA technical memorandum ;0| https://id.loc.gov/authorities/names/n83707893 ;v| X-47.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo2347857| 0;

922 a| BIBCONEWb| 20241125;

922 a| UNREPORTEDPUBSSTAFF;

949 a| Click on web addressw| asish| joyner94;

596 a| 1;

998 a| 6500691;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 6500691-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 12/13/2024x| EDOCUMENTz| JERESOURCE;

Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 / by Cornelius Driver and M. Leroy Spearman.

Author/creator	Driver, Cornelius author.
Other author	Spearman, M. Leroy, author.
Other author	United States. National Aeronautics and Space Administration, issuing body.
Format	Electronic
Publication	Washington : National Aeronautics and Space Administration, September 1959.
Description	1 online resource (28 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo234785
Subjects	Stability of airplanes. Airplanes--Tail surfaces. Aerodynamics, Supersonic.

Series	NASA/TM ; X-47 NASA technical memorandum ; https://id.loc.gov/authorities/names/n83707893 ; X-47. ^A467613
General note	"September 1959."
General note	In scope of the U.S. Government Publishing Office Cataloging and Indexing Program (C&I) and Federal Depository Library Program (FDLP).
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 8).
Source of description	Description based on online resource; title from PDF title page (NASA, viewed Nov. 25, 2024).
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:X-47

Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 / by Cornelius Driver and M. Leroy Spearman.

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