درباره ما
MIL-A-8861B
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T16:50:31Z | |
| date available | 2017-09-04T16:50:31Z | |
| date copyright | 02/07/1986 | |
| date issued | 1986 | |
| identifier other | WOCJDAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/114101 | |
| description abstract | This specification covers the requirements for strength and rigidity for flight loading conditions applicable to airplanes. Intended Use: The requirements of this specification are intended to be used for the structural design of airplanes as affected by inflight loads. | |
| language | English | |
| title | MIL-A-8861B | num |
| title | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS | en |
| type | standard | |
| page | 34 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1986 | |
| contenttype | fulltext | |
| subject keywords | Airplane Strength and Rigidity Flight Loads. | |
| subject keywords | Flight Loads | |
| subject keywords | Airplane Strength and Rigidity. | |
| subject keywords | Loads | |
| subject keywords | Flight | |
| subject keywords | Airplane Strength and Rigidity. | |
| subject keywords | Rigidity | |
| subject keywords | Strength and; Airplane Flight Loads. | |
| subject keywords | Strength and Rigidity; Airplane Flight Loads. |
