Works matching IS 00019240 AND DT 2008 AND VI 112 AND IP 1132
Results: 6
Linear theory of optimum hot air balloon performance - application to Titan.
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- Aeronautical Journal, 2008, v. 112, n. 1132, p. 353, doi. 10.1017/S0001924000002311
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- Article
Aircraft gust load estimation due to atmospheric turbulence under different flight conditions.
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- Aeronautical Journal, 2008, v. 112, n. 1132, p. 345, doi. 10.1017/S000192400000230X
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- Article
Air traffic safety: Continued evolution or a new paradigm?
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- Aeronautical Journal, 2008, v. 112, n. 1132, p. 333
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- Article
The role of drag prediction in combat aircraft design and development.
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- Aeronautical Journal, 2008, v. 112, n. 1132, p. 327, doi. 10.1017/S0001924000002293
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- Article
On the aerodynamics of the Gloster E28139 - a historical perspective.
- Published in:
- Aeronautical Journal, 2008, v. 112, n. 1132, p. 307, doi. 10.1017/S0001924000002281
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- Article
Generic stability and control for aerospace flight vehicle conceptual design.
- Published in:
- Aeronautical Journal, 2008, v. 112, n. 1132, p. 293, doi. 10.1017/S000192400000227X
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- Article