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NASA-RP-1060
Subsonic aircraft: Evolution and the matching of size to performance
Year: 1980
Abstract: Methods for estimating the approximate size, weight, and power of aircraft intended to meet specified performance requirements are presented for both jet-powered and propeller-driven aircraft. The methods are simple and require only the use of a pocket computer for rapid application to specific sizing problems. Application of the methods is illustrated by means of sizing studies of a series of jet-powered and propeller-driven aircraft with varying design constraints. Some aspects of the technical evolution of the airplane from 1918 to the present are also briefly discussed.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:32:34Z | |
| date available | 2017-09-04T18:32:34Z | |
| date copyright | 01/01/1980 | |
| date issued | 1980 | |
| identifier other | JBNKAEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/214702 | |
| description abstract | Methods for estimating the approximate size, weight, and power of aircraft intended to meet specified performance requirements are presented for both jet-powered and propeller-driven aircraft. The methods are simple and require only the use of a pocket computer for rapid application to specific sizing problems. Application of the methods is illustrated by means of sizing studies of a series of jet-powered and propeller-driven aircraft with varying design constraints. Some aspects of the technical evolution of the airplane from 1918 to the present are also briefly discussed. | |
| language | English | |
| title | NASA-RP-1060 | num |
| title | Subsonic aircraft: Evolution and the matching of size to performance | en |
| type | standard | |
| page | 447 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1980 | |
| contenttype | fulltext |