Works matching IS 00019240 AND DT 2006 AND VI 110 AND IP 1107
Results: 6
Active Control of a hybrid actuation system for aircraft vertical fin buffet load alleviation.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1107, p. 315, doi. 10.1017/S000192400001318X
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- Publication type:
- Article
Aeroelastic analysis through linear and non-linear methods: a summary of flutter prediction in the PUMA DARP.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1107, p. 333, doi. 10.1017/S0001924000013208
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- Publication type:
- Article
EPISTLE: High lift system design for low-noise applied to a supersonic aircraft.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1107, p. 327, doi. 10.1017/S0001924000013191
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- Publication type:
- Article
CFD fire simulation of the Swissair Flight 111 in-flight fire — Part II: Fire spread analysis.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1107, p. 303, doi. 10.1017/S0001924000013178
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- Publication type:
- Article
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
Key aerodynamic technologies for aircraft engine nacelles.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1107, p. 265, doi. 10.1017/S0001924000013154
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- Publication type:
- Article