Parametric damage tolerance design of metallic aeronautical stiffened panels.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1182, p. 815, doi. 10.1017/S0001924000007296
- By:
- Publication type:
- Article
Works matching IS 00019240 AND DT 2012 AND VI 116 AND IP 1182
Results: 5
1
2
Shape optimisation in the design of thin-walled shells as components of aerospace structures.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1182, p. 793, doi. 10.1017/S0001924000007284
- By:
- Publication type:
- Article
3
Effect of thickness and angle-of-attack on the aeroelastic stability of supersonic fins.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1182, p. 777, doi. 10.1017/S0001924000007272
- By:
- Publication type:
- Article
4
Operational performance of inlet barrier filters for rotorcraft.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1182, p. 847, doi. 10.1017/S0001924000007314
- By:
- Publication type:
- Article
5
Numerical simulations of the flow through the inlet and isolator of a Mach 4 dual mode scramjet.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1182, p. 833, doi. 10.1017/S0001924000007302
- By:
- Publication type:
- Article