Fidelity enhancement of a rotorcraft simulation model through system identification.
- Published in:
- Aeronautical Journal, 2011, v. 115, n. 1170, p. 453, doi. 10.1017/S0001924000006102
- By:
- Publication type:
- Article
Works matching IS 00019240 AND DT 2011 AND VI 115 AND IP 1170
Results: 6
1
2
Aerodynamic shape optimisation of hovering rotors using compressible CFD.
- Published in:
- Aeronautical Journal, 2011, v. 115, n. 1170, p. 513, doi. 10.1017/S0001924000006151
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- Publication type:
- Article
3
Light gyroplane empennage design considerations.
- Published in:
- Aeronautical Journal, 2011, v. 115, n. 1170, p. 505, doi. 10.1017/S000192400000614X
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- Publication type:
- Article
4
Trailing-edge flap flow control for dynamic stall.
- Published in:
- Aeronautical Journal, 2011, v. 115, n. 1170, p. 493, doi. 10.1017/S0001924000006138
- By:
- Publication type:
- Article
5
Application of aerodynamic model structure determination to UAV data.
- Published in:
- Aeronautical Journal, 2011, v. 115, n. 1170, p. 481, doi. 10.1017/S0001924000006126
- By:
- Publication type:
- Article
6
Flow field and performance analysis of an integrated diverterless supersonic inlet.
- Published in:
- Aeronautical Journal, 2011, v. 115, n. 1170, p. 471, doi. 10.1017/S0001924000006114
- By:
- Publication type:
- Article