Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle
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| Main Author: | |
|---|---|
| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Hampton, Va. : [Springfield, Va. :
National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor,
1994]
|
| Series: | NASA technical memorandum
4574 |
| Subjects: | |
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| 100 | 1 | |a Wing, David J | |
| 245 | 1 | 0 | |a Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle |h [microform] / |c David J. Wing |
| 260 | |a Hampton, Va. : |b National Aeronautics and Space Administration, Langley Research Center ; |a [Springfield, Va. : |b National Technical Information Service, distributor, |c 1994] | ||
| 300 | |a 1 v | ||
| 440 | 0 | |a NASA technical memorandum |v 4574 | |
| 500 | |a Distributed to depository libraries in microfiche | ||
| 500 | |a Shipping list no.: 95-0410-M | ||
| 500 | |a Shipping list no.: 95-0478-M | ||
| 533 | |a Microfiche |b [Washington, D.C. : |c National Aeronautics and Space Administration, |d 1995] |e 3 microfiches. | ||
| 650 | 7 | |a Coanda effect |2 nasat | |
| 650 | 7 | |a Computational fluid dynamics |2 nasat | |
| 650 | 7 | |a Convergent-divergent nozzles |2 nasat | |
| 650 | 7 | |a Flow deflection |2 nasat | |
| 650 | 7 | |a Flow visualization |2 nasat | |
| 650 | 7 | |a Fluidics |2 nasat | |
| 650 | 7 | |a Jet thrust |2 nasat | |
| 650 | 7 | |a Nozzle flow |2 nasat | |
| 650 | 7 | |a Secondary flow |2 nasat | |
| 650 | 7 | |a Static tests |2 nasat | |
| 650 | 7 | |a Thrust vector control |2 nasat | |
| 650 | 7 | |a Two dimensional flow |2 nasat | |
| 650 | 7 | |a Two dimensional models |2 nasat | |
| 650 | 7 | |a Two fluid models |2 nasat | |
| 650 | 7 | |a Wind tunnel tests |2 nasat | |
| 710 | 2 | |a Langley Research Center | |
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