Estimating aerofoil lift from flow angle.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1219, p. 1167, doi. 10.1017/S0001924000011180
- By:
- Publication type:
- Article
Works matching IS 00019240 AND DT 2015 AND VI 119 AND IP 1219
Results: 6
1
2
Total pressure distortion levels at the aerodynamic interface plane of a military aircraft.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1219, p. 1147, doi. 10.1017/S0001924000011179
- By:
- Publication type:
- Article
3
Intake ground vortex and computational modelling of foreign object ingestion.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1219, p. 1123, doi. 10.1017/S0001924000011167
- By:
- Publication type:
- Article
4
Rotorcraft-pilot coupling analysis through state-space aerodynamic modelling.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1219, p. 1105, doi. 10.1017/S0001924000011155
- By:
- Publication type:
- Article
5
Aerodynamic modelling of fin stabilised underslung loads.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1219, p. 1073, doi. 10.1017/S0001924000011143
- By:
- Publication type:
- Article
6
Design, numerical simulation and experimental testing of a controlled electrical actuation system in a real aircraft morphing wing model.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1219, p. 1047, doi. 10.1017/S0001924000011131
- By:
- Publication type:
- Article