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040 a| GPOb| enge| rdae| pnc| GPOd| MvI;

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:210567;

100 1 a| DeBonis, James R.,e| author.=| ^A1099149;

245 10 a| Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system /c| J.R. DeBonis and C.J. Trefny.;

246 3 a| Supersonic wind tunnel tests of a half-axisymmetric 12 degree spike inlet to a rocket-based combined-cycle propulsion system;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Glenn Research Center,c| February 2001.;

300 a| 1 online resource (18 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| 2001-210567;

500 a| "February 2001.";

500 a| "Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting sponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000.";

500 a| "Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.;

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

504 a| Includes bibliographical references (page 5).;

513 a| Technical memorandum.;

536 a| Sponsored by the National Aeronautics and Space Administrationd| WU-523-61-33-00d| E-12533;

588 a| Description based on online resource; title from PDF title page (NASA, viewed Nov. 13, 2017).;

650 7 a| Air breathing boosters.2| nasat;

650 7 a| Hypersonic speed.2| nasat;

650 7 a| Computational fluid dynamics.2| nasat;

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

650 7 a| Propulsion.2| nasat;

650 7 a| Pressure distribution.2| nasat;

700 1 a| Trefny, Charles J.,e| author.=| ^A424429;

710 2 a| NASA Glenn Research Center,e| issuing body.=| ^A420740;

776 08 i| Print version:t| Supersonic Wind Tunnel Tests of a Half-Axisymmetric 12 Deg-Spike Inlet to a Rocket-Based Combined-Cycw| (OCoLC)640923504;

776 08 i| Microfiche version:a| DeBonis, James R.t| Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion systemw| (OCoLC)50765193;

830 0 a| NASA technical memorandumv| 2001-210567.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/LPS23166;

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

596 a| 1;

998 a| 4792447;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4792447-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 12/8/2017x| EDOCUMENTz| JERESOURCE;

Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / J.R. DeBonis and C.J. Trefny.

Author/creator	DeBonis, James R. author.
Other author	Trefny, Charles J., author.
Other author	NASA Glenn Research Center, issuing body.
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2001.
Description	1 online resource (18 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS23166

Variant title	Supersonic wind tunnel tests of a half-axisymmetric 12 degree spike inlet to a rocket-based combined-cycle propulsion system
Series	NASA/TM ; 2001-210567 NASA technical memorandum 2001-210567. ^A467613
General note	"February 2001."
General note	"Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting sponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000."
General note	"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 5).
Report note	Technical memorandum.
Funding information	Sponsored by the National Aeronautics and Space Administration WU-523-61-33-00 E-12533
Source of description	Description based on online resource; title from PDF title page (NASA, viewed Nov. 13, 2017).
Issued in other form	Print version: Supersonic Wind Tunnel Tests of a Half-Axisymmetric 12 Deg-Spike Inlet to a Rocket-Based Combined-Cyc
Issued in other form	Microfiche version: DeBonis, James R. Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:210567

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Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / J.R. DeBonis and C.J. Trefny.

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