Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf /
Saved in:
Main Author: | |
---|---|
Corporate Author: | |
Other Authors: | , |
Format: | Government Document Book |
Language: | English |
Published: |
Hampton, Va. : Springfield, VA :
National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor,
[1996]
Hampton, Va. : Springfield, VA : [1996] |
Series: | NASA technical memorandum
4719. |
Subjects: |
MARC
LEADER | 00000cam a2200000Ka 4500 | ||
---|---|---|---|
001 | 77df5fe7-f185-4e7c-bd57-48e0c7d6afc5 | ||
005 | 20240707000000.0 | ||
008 | 990727s1996 vaua b f000 0 eng d | ||
035 | |a (OCoLC)41964652 | ||
037 | |a 19970001734 |b NASA | ||
040 | |a GPO |b eng |c GPO |d SYB |d OCLCQ |d OCLCO |d GPO |d MvI | ||
049 | |a MNUL | ||
050 | 4 | |a TL521.3.T4 | |
074 | |a 0830-D (MF) | ||
086 | 0 | |a NAS 1.15:4719 | |
099 | |a NAS 1.15:4719 | ||
100 | 1 | |a Lamb, Milton. | |
245 | 1 | 0 | |a Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf / |c Milton Lamb and John G. Taylor, Mark C. Frassinelli. |
260 | |a Hampton, Va. : |b National Aeronautics and Space Administration, Langley Research Center ; |a Springfield, VA : |b National Technical Information Service, distributor, |c [1996] | ||
264 | 1 | |a Hampton, Va. : |b National Aeronautics and Space Administration, Langley Research Center ; |a Springfield, VA : |b National Technical Information Service, distributor, |c [1996] | |
300 | |a iii, 103 pages : |b illustrations. | ||
336 | |a text |b txt |2 rdacontent | ||
337 | |a microform |b h |2 rdamedia | ||
338 | |a microfiche |b he |2 rdacarrier | ||
490 | 1 | |a NASA technical memorandum ; |v 4719 | |
500 | |a Shipping list no.: 99-0685-M. | ||
533 | |a Microfiche. |b [Washington, D.C. : |c National Aeronautics and Space Administration, |d 1997]. |e 2 microfiches. | ||
650 | 0 | |a Aerodynamic load. | |
630 | 0 | 0 | |a Collection Plumes |
650 | 0 | |a Airframes. | |
650 | 7 | |a Convergent-divergent nozzles. |2 nasat | |
650 | 7 | |a Pressure ratio. |2 nasat | |
650 | 7 | |a Pressure distribution. |2 nasat | |
650 | 7 | |a Throats. |2 nasat | |
650 | 7 | |a Static tests. |2 nasat | |
650 | 7 | |a Plumes. |2 nasat | |
650 | 7 | |a Nozzle design. |2 nasat | |
650 | 7 | |a Afterburning. |2 nasat | |
650 | 7 | |a Aircraft structures. |2 nasat | |
650 | 7 | |a Two dimensional flow. |2 nasat | |
650 | 7 | |a Two dimensional models. |2 nasat | |
700 | 1 | |a Taylor, John G. | |
700 | 1 | |a Frassinelli, Mark C. | |
710 | 2 | |a Langley Research Center. | |
776 | 0 | 8 | |i Print version: |a Lamb, Milton. |t Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf |w (OCoLC)35835164 |
776 | 0 | 8 | |i Online version: |a Lamb, Milton. |t Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf |w (OCoLC)755200823 |
830 | 0 | |a NASA technical memorandum |v 4719. | |
999 | 1 | 0 | |i 77df5fe7-f185-4e7c-bd57-48e0c7d6afc5 |l 9942847100001701 |s US-MNU |m static_internal_performance_of_a_two_dimensional_convergent_divergent______1996_______natioa________________________________________lamb__milton_______________________nas_1_15_4719p |