Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2 / Francis J. Capone ; Langley Research Center, Hampton, Va.
| Author/creator | Capone, Francis J. |
| Other author | Langley Research Center. |
| Format | Book |
| Publication Info | Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1976. |
| Description | [1], 205 p. : ill. ; 27 cm. |
| Subjects |
| Series | NASA technical memorandum ; NASA TM X-3313 NASA technical memorandum NASA TM X-3313. ^A467613 |
| General note | Cover title. |
| Bibliography note | Bibliography: p. 18. |
| GPO item number | 830-D |
| Govt. docs number | NAS 1.15:X-3313 |
Availability
| Library | Location | Call Number | Status | Item Actions |
|---|---|---|---|---|
| Joyner | Fed Docs Stacks | ASK AT REFERENCE DESK | ✔ Available | Place Hold |