Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients /
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| Author / Creator: | Sanders, Bobby W., author. |
|---|---|
| Imprint: | Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980. |
| Description: | 1 online resource (iii, 98 pages) : illustrations. |
| Language: | English |
| Series: | NASA technical paper ; 1531 NASA technical paper ; 1531. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/10292775 |
MARC
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| 040 | |a OCLCE |b eng |e rda |e pn |c OCLCE |d OCLCQ |d OCLCF |d OCLCQ |d GPO |d MvI | ||
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| 100 | 1 | |a Sanders, Bobby W., |e author. |0 http://id.loc.gov/authorities/names/n81131070 |1 http://viaf.org/viaf/1342108 | |
| 245 | 1 | 0 | |a Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients / |c Bobby W. Sanders. |
| 264 | 1 | |a Washington, District of Columbia : |b National Aeronautics and Space Administration, Scientific and Technical Information Office, |c January 1980. | |
| 300 | |a 1 online resource (iii, 98 pages) : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a computer |b c |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/c | ||
| 338 | |a online resource |b cr |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/cr | ||
| 490 | 1 | |a NASA technical paper ; |v 1531 | |
| 500 | |a Title from title screen (viewed Sept. 22, 2014). | ||
| 500 | |a "January 1980." | ||
| 500 | |a "Performing organization, Lewis Research Center"--Technical report documentation page. | ||
| 504 | |a Includes bibliographical references (pages 27-28). | ||
| 536 | |a Sponsored by National Aeronautics and Space Administration |h 505-04 | ||
| 536 | |d E-9467 | ||
| 650 | 0 | |a Airplanes |x Turbojet engines |x Air intakes. |0 http://id.loc.gov/authorities/subjects/sh85002909 | |
| 650 | 0 | |a Airplanes |x Motors |x Valves. |0 http://id.loc.gov/authorities/subjects/sh85002862 | |
| 650 | 7 | |a Aerodynamic stability. |2 nasat | |
| 650 | 7 | |a Bypasses. |2 nasat | |
| 650 | 7 | |a Propulsion system performance. |2 nasat | |
| 650 | 7 | |a Supersonic inlets. |2 nasat | |
| 650 | 7 | |a Turbojet engines. |2 nasat | |
| 650 | 7 | |a Wind tunnel stability tests. |2 nasat | |
| 650 | 7 | |a Airplanes |x Motors |x Valves. |2 fast |0 (OCoLC)fst00803359 | |
| 650 | 7 | |a Airplanes |x Turbojet engines |x Air intakes. |2 fast |0 (OCoLC)fst00803511 | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration. |b Scientific and Technical Information Office, |e issuing body. |0 http://id.loc.gov/authorities/names/n78091121 |1 http://viaf.org/viaf/125975314 | |
| 710 | 2 | |a Lewis Research Center, |e author. |0 http://id.loc.gov/authorities/names/n80126316 |1 http://viaf.org/viaf/155061179 | |
| 776 | 0 | 8 | |i Print version: |a Sanders, Bobby W. |t Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controled inlet-stability bypass system when subjected to internal and external airflow transients |w (OCoLC)7959956 |
| 830 | 0 | |a NASA technical paper ; |v 1531. | |
| 856 | 4 | 0 | |u http://purl.fdlp.gov/GPO/gpo52217 |y GPO Documents Without Shelves |
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| 929 | |a eresource | ||
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| 928 | |t Library of Congress classification |l Online |c UC-FullText |u http://purl.fdlp.gov/GPO/gpo52217 |z GPO Documents Without Shelves |g ebooks |i 8444643 | ||