Sub boundary-layer vortex generators for the control of shock induced separation.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1106, p. 215, doi. 10.1017/S0001924000001196
- By:
- Publication type:
- Article
Works matching IS 00019240 AND DT 2006 AND VI 110 AND IP 1106
Results: 9
1
2
Fundamentals of Multibody Dynamics: Theory and Applications.
- Published in:
- 2006
- By:
- Publication type:
- Book Review
3
Numerical calculation of separated flow past square and rectangular cylinders using panel technique.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1106, p. 249, doi. 10.1017/S0001924000001226
- By:
- Publication type:
- Article
4
An analysis of exit availability, exit usage and passenger exit selection behaviour exhibited during actual aviation accidents.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1106, p. 239, doi. 10.1017/S0001924000001214
- By:
- Publication type:
- Article
5
Impacts of low-pressure (LP) compressor's deterioration upon an aero-engine's high-pressure (HP) turbine blade's life consumption.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1106, p. 227, doi. 10.1017/S0001924000001202
- By:
- Publication type:
- Article
6
Corporate memory contribution to integrated design and analysis systems.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1106, p. 257, doi. 10.1017/S0001924000001238
- By:
- Publication type:
- Article
7
Applied Orbit Perturbation and Maintenance.
- Published in:
- 2006
- By:
- Publication type:
- Book Review
8
Radar and Laser Cross Section Engineering — Second edition.
- Published in:
- 2006
- By:
- Publication type:
- Book Review
9
Impact of privatisation on the financial and economic performance of European airports.
- Published in:
- Aeronautical Journal, 2006, v. 110, n. 1106, p. 197, doi. 10.1017/S0001924000001184
- By:
- Publication type:
- Article