Jet-induced effects the aerodynamics of jet- and fan-powered V/STOL aircraft in hover and transition /
I tiakina i:
| Kaituhi matua: | |
|---|---|
| Kaituhi rangatōpū: | |
| Ētahi atu kaituhi: | , |
| Hōputu: | Tāhiko īPukapuka |
| Reo: | Ingarihi |
| I whakaputaina: |
Reston, Va. :
American Institute of Aeronautics and Astronautics, Inc.,
c2006.
|
| Rangatū: | Progress in astronautics and aeronautics ;
v. 217. |
| Ngā marau: | |
| Urunga tuihono: | An electronic book accessible through the World Wide Web; click to view |
| Ngā Tūtohu: |
Kāore He Tūtohu, Me noho koe te mea tuatahi ki te tūtohu i tēnei pūkete!
|
MARC
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| 020 | |z 1563478412 | ||
| 020 | |z 9781563478413 | ||
| 020 | |z 9781600864674 (e-book) | ||
| 035 | |a (CaPaEBR)ebr10516622 | ||
| 035 | |a (OCoLC)608694761 | ||
| 040 | |a CaPaEBR |c CaPaEBR | ||
| 050 | 1 | 4 | |a TL685 |b .K84 2006eb |
| 082 | 0 | 4 | |a 629.133/35 |2 22 |
| 100 | 1 | |a Kuhn, Richard E. | |
| 245 | 1 | 0 | |a Jet-induced effects |h [electronic resource] : |b the aerodynamics of jet- and fan-powered V/STOL aircraft in hover and transition / |c Richard E. Kuhn, Richard J. Margason, Peter Curtis. |
| 260 | |a Reston, Va. : |b American Institute of Aeronautics and Astronautics, Inc., |c c2006. | ||
| 300 | |a xi, 203 p. : |b ill. | ||
| 490 | 1 | |a Progress in astronautics and aeronautics ; |v v. 217 | |
| 504 | |a Includes bibliographical references and index. | ||
| 533 | |a Electronic reproduction. |b Palo Alto, Calif. : |c ebrary, |d 2013. |n Available via World Wide Web. |n Access may be limited to ebrary affiliated libraries. | ||
| 650 | 0 | |a Vertically rising aircraft |x Aerodynamics. | |
| 655 | 7 | |a Electronic books. |2 local | |
| 700 | 1 | |a Margason, Richard J. | |
| 700 | 1 | |a Curtis, Peter. | |
| 710 | 2 | |a ebrary, Inc. | |
| 830 | 0 | |a Progress in astronautics and aeronautics ; |v v. 217. | |
| 856 | 4 | 0 | |u http://site.ebrary.com/lib/daystar/Doc?id=10516622 |z An electronic book accessible through the World Wide Web; click to view |
| 908 | |a 170314 | ||
| 942 | 0 | 0 | |c EB |
| 999 | |c 131971 |d 131971 | ||