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035 a| (Sirsi) o761192031;

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:X-116;

100 1 a| Driver, Cornelius,e| author.=| ^A1438444;

245 10 a| Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 /c| by Cornelius Driver.;

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

300 a| 1 online resource (47 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-116;

500 a| "September 1959"--Cover.;

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

504 a| Includes bibliographical references (page 6).;

513 a| Technical memorandum.;

588 a| Description based on online resource; title from PDF cover, (NASA, viewed on May 26, 2022).;

650 7 a| Hypersonic aircraft.2| nasat;

650 7 a| Aerodynamic characteristics.2| nasat;

650 0 a| Aerodynamics.=| ^A48226;

650 0 a| Aerodynamic measurements.=| ^A593564;

650 0 a| Mach number.=| ^A368195;

650 0 a| Hypersonic planes.=| ^A242333;

650 0 a| Wind tunnel testing.=| ^A782018;

650 0 a| Shells (Engineering)=| ^A53809;

650 0 a| Noses (Aircraft)=| ^A485666;

710 1 a| United States.b| National Aeronautics and Space Administratione| issuing body.=| ^A5437;

776 08 i| Print version:a| Driver, Corneliust| Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86w| (OCoLC)688628077;

830 0 a| NASA technical memorandum ;v| X-116.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo1828547| 0;

922 a| BIBCONEWb| 20220526;

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

596 a| 1;

998 a| 5826425;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 5826425-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 6/13/2022x| EDOCUMENTz| JERESOURCE;

Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 / by Cornelius Driver.

Author/creator	Driver, Cornelius 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 (47 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo182854
Subjects	Aerodynamics. Aerodynamic measurements. Mach number. Hypersonic planes. Wind tunnel testing. Shells (Engineering) Noses (Aircraft)

Series	NASA/TM; ; X-116 NASA technical memorandum ; X-116. ^A467613
General note	"September 1959"--Cover.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 6).
Report note	Technical memorandum.
Source of description	Description based on online resource; title from PDF cover, (NASA, viewed on May 26, 2022).
Issued in other form	Print version: Driver, Cornelius Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:X-116

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Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 / by Cornelius Driver.

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