Numerical evaluation of the aerodynamic influence of the helicopter composite blade trailing edge tabs.
- Published in:
- Archive of Applied Mechanics, 2007, v. 77, n. 12, p. 893, doi. 10.1007/s00419-007-0133-1
- By:
- Publication type:
- Article
Works matching IS 09391533 AND DT 2007 AND VI 77 AND IP 12
Results: 5
1
2
Effect of parameters on the rubbing condition of an unbalanced rotor system with initial permanent deflection.
- Published in:
- Archive of Applied Mechanics, 2007, v. 77, n. 12, p. 883, doi. 10.1007/s00419-007-0134-0
- By:
- Publication type:
- Article
3
Solutions to a limited-permeable crack or two limited-permeable collinear cracks in piezoelectric/piezomagnetic materials.
- Published in:
- Archive of Applied Mechanics, 2007, v. 77, n. 12, p. 861, doi. 10.1007/s00419-007-0135-z
- By:
- Publication type:
- Article
4
Vibrational dynamics of modern lightrail modules.
- Published in:
- Archive of Applied Mechanics, 2007, v. 77, n. 12, p. 849, doi. 10.1007/s00419-007-0130-4
- Publication type:
- Article
5
An inverse algorithm for the identification and the sensitivity analysis of the parameters governing micropolar elasto-plastic granular material.
- Published in:
- Archive of Applied Mechanics, 2007, v. 77, n. 12, p. 911, doi. 10.1007/s00419-007-0162-9
- By:
- Publication type:
- Article