Time-linearised transonic computations including entropy, vorticity and shock wave motion effects.
- Published in:
- Aeronautical Journal, 2003, v. 107, n. 1077, p. 687, doi. 10.1017/s0001924000013555
- By:
- Publication type:
- Article
Works matching IS 00019240 AND DT 2003 AND VI 107 AND IP 1077
Results: 5
1
2
Non-linearities in flight control systems.
- Published in:
- Aeronautical Journal, 2003, v. 107, n. 1077, p. 673, doi. 10.1017/s0001924000013543
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- Publication type:
- Article
3
Reduction of helicopter vibration through cyclic control of variable orifice dampers.
- Published in:
- Aeronautical Journal, 2003, v. 107, n. 1077, p. 657, doi. 10.1017/s0001924000013531
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- Publication type:
- Article
4
Aerospace applications of luminescent paint. Part two: Heat transfer measurement.
- Published in:
- Aeronautical Journal, 2003, v. 107, n. 1077, p. 649, doi. 10.1017/s000192400001352x
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- Publication type:
- Article
5
Aerospace applications of luminescent paint. Part one: Pressure measurement.
- Published in:
- Aeronautical Journal, 2003, v. 107, n. 1077, p. 637, doi. 10.1017/s0001924000013518
- By:
- Publication type:
- Article