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ADS-10C-SP
AIR VEHICLE TECHNICAL DESCRIPTION
Organization:
ARMY - AV - Aviation and Missile Command
Year: 2000
Abstract: This standard practice Aeronautical Design Standard specifies the air vehicle technical data necessary to perform a detailed analysis of the performance, handling qualities, rotor dynamics, airframe dynamics, and acoustics of proposed new development or derivative rotorcraft. It is the purpose of this standard to provide a clear technical description of the proposed air vehicle and its components at a level of detail consistent with the current stage of its design. To this end, the data requirements are divided into topics and the topics are divided into three levels: Level I, Level II, and Level III. Level I (minimum) requires sufficient information to conduct a basic performance and stability and control analysis including the aerodynamic effects of the rotor system and the fuselage. Level II (intermediate) requires all of the data required for Level I plus additional data required for more detailed rotor and fuselage aerodynamics and a basic dynamic analysis of the rotors and the fuselage. Level III (detailed) is intended to allow a very detailed aerodynamic and dynamic analysis.
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| contributor author | ARMY - AV - Aviation and Missile Command | |
| date accessioned | 2017-09-04T18:03:02Z | |
| date available | 2017-09-04T18:03:02Z | |
| date copyright | 03/13/2000 | |
| date issued | 2000 | |
| identifier other | GDGOPAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jse/handle/yse/185987 | |
| description abstract | This standard practice Aeronautical Design Standard specifies the air vehicle technical data necessary to perform a detailed analysis of the performance, handling qualities, rotor dynamics, airframe dynamics, and acoustics of proposed new development or derivative rotorcraft. It is the purpose of this standard to provide a clear technical description of the proposed air vehicle and its components at a level of detail consistent with the current stage of its design. To this end, the data requirements are divided into topics and the topics are divided into three levels: Level I, Level II, and Level III. Level I (minimum) requires sufficient information to conduct a basic performance and stability and control analysis including the aerodynamic effects of the rotor system and the fuselage. Level II (intermediate) requires all of the data required for Level I plus additional data required for more detailed rotor and fuselage aerodynamics and a basic dynamic analysis of the rotors and the fuselage. Level III (detailed) is intended to allow a very detailed aerodynamic and dynamic analysis. | |
| language | English | |
| title | ADS-10C-SP | num |
| title | AIR VEHICLE TECHNICAL DESCRIPTION | en |
| type | standard | |
| page | 26 | |
| status | Active | |
| tree | ARMY - AV - Aviation and Missile Command:;2000 | |
| contenttype | fulltext |