Aeroelastic analysis through linear and non-linear methods: a summary of flutter prediction in the PUMA DARP.
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- Aeronautical Journal, 2006, v. 110, n. 1107, p. 333, doi. 10.1017/S0001924000013208
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- Article
Works matching DE "MODEL airplane aerodynamics"
Results: 5
1
2
EPISTLE: High lift system design for low-noise applied to a supersonic aircraft.
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- Aeronautical Journal, 2006, v. 110, n. 1107, p. 327, doi. 10.1017/S0001924000013191
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- Publication type:
- Article
3
Active Control of a hybrid actuation system for aircraft vertical fin buffet load alleviation.
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- Aeronautical Journal, 2006, v. 110, n. 1107, p. 315, doi. 10.1017/S000192400001318X
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- Publication type:
- Article
4
Rigid body separation dynamics for space launch vehicles.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1107, p. 289, doi. 10.1017/S0001924000013166
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- Publication type:
- Article
5
Simulation and flight test of a temperature sensing stabilisation system.
- Published in:
- Aeronautical Journal, 2005, v. 109, n. 1094, p. 167, doi. 10.1017/S0001924000000671
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- Publication type:
- Article