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NASA-TN-D-30
Flight Investigation of the Lift and Drag Characteristics of a Swept-Wing, Multijet, Transport-Type Airplane
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:21:30Z | |
| date available | 2017-09-04T15:21:30Z | |
| date copyright | 01/01/1960 | |
| date issued | 1960 | |
| identifier other | MZHOEEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/21466 | |
| description abstract | The lift and drag characteristics of a Boeing KC-135 airplane were determined during maneuvering flight over the Mach number range from 0.70 to 0.85 for the airplane in the clean configuration at an altitude of 26,000 feet. Data were also obtained over the speed range of 130 knots to 160 knots at 9,000 feet for various flap deflections with gear down. | |
| language | English | |
| title | NASA-TN-D-30 | num |
| title | Flight Investigation of the Lift and Drag Characteristics of a Swept-Wing, Multijet, Transport-Type Airplane | en |
| type | standard | |
| page | 30 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1960 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC CHARACTERISTICS | |
| subject keywords | AERODYNAMIC COEFFICIENTS | |
| subject keywords | AERODYNAMIC CONFIGURATIONS | |
| subject keywords | AERODYNAMIC DRAG | |
| subject keywords | C-135 AIRCRAFT | |
| subject keywords | FLIGHT TESTS | |
| subject keywords | JET AIRCRAFT | |
| subject keywords | LIFT | |
| subject keywords | MACH NUMBER | |
| subject keywords | MANEUVERS | |
| subject keywords | SUBSONIC SPEED | |
| subject keywords | SWEPT WINGS |
