论文信息 - Separation Control for Rotorcraft Final Progress Report - 字舞流文

Separation Control for Rotorcraft Final Progress Report

Brian E. Wake | Razvan Florea | Peter F. Lorber | Duane C. McCormick | B. Wake | D. Mccormick | P. Lorber | R. Florea

[1] Peter Lorber,et al. Compressibility effects on the dynamic stall of a three-dimensional wing , 1992 .

[2] Michael S. Torok,et al. Techniques for Comprehensive Measurement of Model Helicopter Rotor Aerodynamics , 1994 .

[3] Peter F. Lorber,et al. Airfoil dynamic stall at constant pitch rate and high Reynolds number , 1987 .

[4] B. Nishri,et al. The delay of turbulent boundary layer separation by oscillatory active control , 1989 .

[5] L. Carr,et al. Compressibility effects on dynamic stall , 1996 .

[6] U. Ingard. On the Theory and Design of Acoustic Resonators , 1953 .

[7] Patrick Reisenthel,et al. Control of Separated Flows Using Forced Unsteadiness , 1985 .

[8] A. Seifert,et al. Oscillatory Control of Separation at High Reynolds Numbers , 1999 .

[9] William G. Bousman,et al. A Qualitative Examination of Dynamic Stall from Flight Test Data , 1997 .

[10] Israel J Wygnanski,et al. Parameters affecting dynamic stall control by oscillatory excitation , 1999 .