Issac, Jason Cherian Ses in Transonic Flow

by National Aeronautics and Space Administration

Flutter analysis of a two degree of freedom airfoil in compressible flow is performed using a state-space representation of the unsteady aerodynamic behavior. Indicial response functions are used to represent the normal force and moment response of the airfoil. The structural equations of motion of the airfoil with bending and torsional degrees of freedom are coupled to the unsteady air loads and the aeroelastic system so modelled is solved as an...

• Format: Paperback
• Language: English
• ISBN: 1730888860
• ISBN13: 9781730888861
• Release Date: January 1
• Publisher: Independently Published
• Length: 82 Pages
• Weight: 0.47 lbs.
• Dimensions: 0.2" x 8.5" x 11.0"