Publisher's Synopsis
A summary of the work performed under NASA grant NCC3-605 is presented. More details can be found in the cited references. This grant led to the development of relatively faster aeroelastic analyses methods for predicting flutter and forced response in fans, compressors, and turbines using computational fluid dynamic (CFD) methods.Keith, Theo G., Jr. and Reddy, T. S. R.Glenn Research CenterAEROELASTICITY; AERODYNAMIC STABILITY; ROTATING BODIES; AIRCRAFT STRUCTURES; PREDICTIONS; FLUTTER; FLUTTER ANALYSIS; FANS; TURBINES; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; THREE DIMENSIONAL MODELS...
