Vortex breakdown location over 65° delta wings empiricism and experiment.
- Published in:
- Aeronautical Journal, 2004, v. 108, n. 1087, p. 475, doi. 10.1017/S0001924000000294
- By:
- Publication type:
- Article
Works matching IS 00019240 AND DT 2004 AND VI 108 AND IP 1087
Results: 5
1
2
Design methodology and performance of an indraft wind tunnel.
- Published in:
- Aeronautical Journal, 2004, v. 108, n. 1087, p. 465, doi. 10.1017/S0001924000000282
- By:
- Publication type:
- Article
3
A question of survival — military aircraft vs the electromagnetic environment.
- Published in:
- Aeronautical Journal, 2004, v. 108, n. 1087, p. 453, doi. 10.1017/S0001924000000270
- By:
- Publication type:
- Article
4
Recent developments in delta wing aerodynamics.
- Published in:
- Aeronautical Journal, 2004, v. 108, n. 1087, p. 437, doi. 10.1017/S0001924000000269
- By:
- Publication type:
- Article
5
Investigation of active control of swept shock wave/turbulent boundary-layer interactions — PSP results.
- Published in:
- Aeronautical Journal, 2004, v. 108, n. 1087, p. 483, doi. 10.1017/S0001924000000300
- By:
- Publication type:
- Article