Aeroelastic Response Analysis of Composite Blades Based on Geometrically Exact Beam Theory.
- Published in:
- Journal of the American Helicopter Society, 2019, v. 64, n. 2, p. 1, doi. 10.4050/JAHS.64.022007
- By:
- Publication type:
- Article
Works matching IS 00028711 AND DT 2019 AND VI 64 AND IP 2
Results: 7
1
2
Generalized Aerodynamic Optimization of Hovering Coaxial Rotor Blades.
- Published in:
- Journal of the American Helicopter Society, 2019, v. 64, n. 2, p. 1, doi. 10.4050/JAHS.64.022006
- By:
- Publication type:
- Article
3
The Tip Vortex System of a Four-Bladed Rotor in Dynamic Stall Conditions.
- Published in:
- Journal of the American Helicopter Society, 2019, v. 64, n. 2, p. 1, doi. 10.4050/JAHS.64.022005
- By:
- Publication type:
- Article
4
Performance and Loads of a Lift Offset Rotor: Hover andWind Tunnel Testing.
- Published in:
- Journal of the American Helicopter Society, 2019, v. 64, n. 2, p. 1, doi. 10.4050/JAHS.64.022002
- By:
- Publication type:
- Article
5
Helicopter Fuselage Model Drag Reduction by Active Flow Control Systems.
- Published in:
- Journal of the American Helicopter Society, 2019, v. 64, n. 2, p. 1, doi. 10.4050/JAHS.64.022001
- By:
- Publication type:
- Article
6
Progressive Fatigue Damage Simulation in Laminated Composites Based on Explicit Finite Element Formulation.
- Published in:
- Journal of the American Helicopter Society, 2019, v. 64, n. 2, p. 1, doi. 10.4050/JAHS.64.022004
- By:
- Publication type:
- Article
7
ACT/FHS System Identification Including Rotor and Engine Dynamics.
- Published in:
- Journal of the American Helicopter Society, 2019, v. 64, n. 2, p. 1, doi. 10.4050/JAHS.64.022003
- By:
- Publication type:
- Article