Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition / John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009.
| Author/creator | Slater, John W. |
| Other author | Saunders, John D. |
| Other author | NASA Glenn Research Center. |
| Other author | AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference 2009 : Bremen, Germany) |
| Format | Electronic |
| Publication Info | Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] |
| Description | 1 online resource (27 p.) : ill. |
| Supplemental Content | https://purl.fdlp.gov/GPO/gpo4610 |
| Series | NASA/TM ; 2010-216362 NASA technical memorandum 216362. ^A467613 |
| General note | Title from title screen (viewed on March 3, 2011). |
| General note | "May 2010." |
| General note | "AIAA-2009-7349." |
| General note | GPO Cataloging Record Distribution Program (CRDP). |
| Bibliography note | Includes bibliographical references (p. 27) |
| Funding information | WBS 138494.04.01.01 |
| GPO item number | 0830-D (online) |
| Govt. docs number | NAS 1.15:2010-216362 |
Availability
| Library | Location | Call Number | Status | Item Actions |
|---|---|---|---|---|
| Electronic Resources | Access Content Online | ✔ Available |