Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊/
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| Main Author: | |
|---|---|
| Corporate Author: | |
| Format: | Government Document eBook |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
February 1985.
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| Series: | NASA technical paper ;
2391. |
| Subjects: | |
| Online Access: | CONNECT CONNECT |
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| 100 | 1 | |a Leavitt, Laurence D., |e author. | |
| 245 | 1 | 0 | |a Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊/ |c Laurence D. Leavitt. |
| 264 | 1 | |a Washington, D.C. : |b National Aeronautics and Space Administration, Scientific and Technical Information Branch, |c February 1985. | |
| 300 | |a 1 online resource (66 pages) : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent | ||
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| 490 | 1 | |a NASA/TP ; |v 2391 | |
| 500 | |a "February 1985." | ||
| 504 | |a Includes bibliographical references (pages 7-8). | ||
| 513 | |a Technical paper. | ||
| 588 | |a Description based on online resource, PDF version; title from title page (NASA, viewed Aug. 23, 2018). | ||
| 650 | 7 | |a Convergent. |2 nasat | |
| 650 | 7 | |a Thrust vector control. |2 nasat | |
| 650 | 7 | |a Wind tunnel tests. |2 nasat | |
| 650 | 7 | |a Nozzle flow. |2 nasat | |
| 650 | 7 | |a Transonic wind tunnels. |2 nasat | |
| 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 Microfiche version: |a Leavitt, Laurence D. |t Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60°. |d [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985 |w (OCoLC)56497170 |
| 830 | 0 | |a NASA technical paper ; |v 2391. | |
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