A simplified model for detonation based pressure-gain combustors [electronic resource] / Daniel E. Paxson ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010.
Saved in:
| Online Access: |
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|---|---|
| Main Author: | |
| Corporate Authors: | , |
| Format: | Government Document Electronic Conference Proceeding eBook |
| Language: | English |
| Published: |
Cleveland, Ohio :
National Aeronautics and Space Administration, Glenn Research Center,
[2010]
|
| Series: | NASA technical memorandum ;
216821. |
| Subjects: |
MARC
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| 100 | 1 | |a Paxson, Daniel E. |0 http://id.loc.gov/authorities/names/no2007084962. | |
| 245 | 1 | 2 | |a A simplified model for detonation based pressure-gain combustors |h [electronic resource] / |c Daniel E. Paxson ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010. |
| 264 | 1 | |a Cleveland, Ohio : |b National Aeronautics and Space Administration, Glenn Research Center, |c [2010] | |
| 300 | |a 1 online resource (13 pages) : |b illustrations, color. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
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| 490 | 1 | |a NASA/TM ; |v 2010-216821. | |
| 500 | |a Title from title screen (viewed on June 13, 2011) | ||
| 500 | |a "November 2010." | ||
| 504 | |a Includes bibliographical references (pages 12-13) | ||
| 500 | |a "AIAA-2010-6717." | ||
| 536 | |h WBS 561581.02.08.03.13.05. | ||
| 650 | 7 | |a Detonation. |2 nasat. | |
| 650 | 7 | |a Gas turbines. |2 nasat. | |
| 650 | 7 | |a Pulsed jet engines. |2 nasat. | |
| 650 | 7 | |a Combustion chambers. |2 nasat. | |
| 650 | 7 | |a Flow distribution. |2 nasat. | |
| 650 | 7 | |a Reliability analysis. |2 nasat. | |
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