Method for the solution of the aeroelastic response problem for rotating wings-Reference-Cited by-同舟云学术

Method for the solution of the aeroelastic response problem for rotating wings

Published:1966-11 Issue:3 Volume:4 Page:445-489
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Piziali R.A.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference14 articles.

1. TCREC TR 62-44;Piziali;A method for computing rotary wing airload distribution in forward flight,1962

2. Computations of rotary wing harmonic sirloads and comparison with experimental results;Piziali,1962

3. Rotor airloads;Piziali,1963

4. Computed induced velocity, induced drag, and angle of attack distributions for a two-bladed rotor;Piziali,1963

5. Engineering Division Giravions Dorand Company Report No. DE 2012;Tararine;Experimental and theoretical study of local induced velocities over a rotor disc for analytical evaluation of the primary loads acting on helicopter rotor blades,1960

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