Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap /
Saved in:
Main Authors: | , |
---|---|
Corporate Author: | |
Format: | Government Document eBook |
Language: | English |
Published: |
Washington, D.C. :
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
April 1986.
|
Series: | NASA technical paper ;
2549. |
Subjects: | |
Online Access: | CONNECT CONNECT |
LEADER | 02899nam a2200625 i 4500 | ||
---|---|---|---|
001 | mig00005109139 | ||
003 | OCoLC | ||
005 | 20180713102507.0 | ||
006 | m o d f | ||
007 | cr bn||||||abp | ||
008 | 120408e198604 dcua obt f000 0 eng c | ||
019 | |a 761237413 | ||
035 | 0 | 0 | |a ocn785283276 |
040 | |a OCLCE |b eng |e rda |e pn |c OCLCE |d OCLCQ |d OCLCO |d OCLCF |d OCLCQ |d GPO |d MvI | ||
042 | |a pcc | ||
049 | |a TXME | ||
074 | |a 0830-H-15 (online) | ||
086 | 0 | |a NAS 1.60:2549 | |
099 | |a Online Government Document | ||
100 | 1 | |a Re, Richard J., |e author. | |
245 | 1 | 0 | |a Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap / |c Richard J. Re and Laurence D. Leavitt. |
264 | 1 | |a Washington, D.C. : |b National Aeronautics and Space Administration, Scientific and Technical Information Branch, |c April 1986. | |
300 | |a 1 online resource (110 pages) : |b illustrations. | ||
336 | |a text |b txt |2 rdacontent | ||
337 | |a computer |b c |2 rdamedia | ||
338 | |a online resource |b cr |2 rdacarrier | ||
490 | 1 | |a NASA/TP ; |v 2549 | |
500 | |a "March 1982." | ||
504 | |a Includes bibliographical references (pages 15-16). | ||
513 | |a Technical paper. | ||
536 | |a Langley Research Center |d L-16025 |d 505-43-90-07 | ||
588 | |a Description based on online resource, PDF version; title from title page (NASA, viewed July 13, 2018). | ||
650 | 7 | |a Static tests. |2 nasat | |
650 | 7 | |a Thrust vector control. |2 nasat | |
650 | 7 | |a Thrust reversal. |2 nasat | |
650 | 7 | |a Wind tunnel tests. |2 nasat | |
650 | 7 | |a Nozzle geometry. |2 nasat | |
650 | 0 | |a Jet nozzles. | |
650 | 0 | |a Jet planes |x Thrust reversers. | |
650 | 7 | |a Jet nozzles. |2 fast |0 (OCoLC)fst00982414 | |
650 | 7 | |a Jet planes |x Thrust reversers. |2 fast |0 (OCoLC)fst00982447 | |
700 | 1 | |a Leavitt, Laurence D., |e author. | |
710 | 1 | |a United States. |b National Aeronautics and Space Administration. |b Scientific and Technical Information Branch, |e issuing body. | |
710 | 2 | |a Langley Research Center. | |
776 | 0 | 8 | |i Print version: |a Re, Richard J |t Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap |w (OCoLC)36791317 |
776 | 0 | 8 | |i Microfiche: |a Re, Richard J |t Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap |w (OCoLC)56611199 |
830 | 0 | |a NASA technical paper ; |v 2549. | |
856 | 4 | 0 | |z CONNECT |u https://purl.fdlp.gov/GPO/gpo105836 |t 0 |
907 | |a 4111488 |b 06-10-21 |c 12-13-19 | ||
998 | |a wi |b 12-13-19 |c m |d z |e - |f eng |g dcu |h 0 |i 1 | ||
910 | |a MTSUM2018Jan-DecJoined | ||
910 | |a DWS | ||
999 | f | f | |i 948ade8f-533a-4272-a902-5d6f453326da |s e0ffb2c2-3bf3-4193-8d23-7ad076a85ed8 |t 0 |
952 | f | f | |t 1 |e NAS 1.60:2549 |h Library of Congress classification |
856 | 4 | 0 | |t 0 |u https://purl.fdlp.gov/GPO/gpo105836 |z CONNECT |