Correlation of Puma airloads: Evaluation of CFD prediction methods
暂无分享,去创建一个
Alan Jones | Roger C. Strawn | Judith Miller | Andre Desopper | R. Strawn | A. Desopper | A. Jones | Judith E. Miller
[1] C. Tung,et al. Numerical solution of the full-potential equation for rotors and oblique wings using a new wake model , 1985 .
[2] J. Steger,et al. A conservative finite difference algorithm for the unsteady transonic potential equation in generalized coordinates , 1982 .
[3] Gloria K. Yamauchi,et al. Correlation of SA349/2 helicopter flight-test data with a comprehensive rotorcraft model , 1988 .
[4] W. R. Johnson,et al. The Prediction of Transonic Flows on an Advancing Rotor , 1986 .
[5] W. Johnson,et al. Development of a comprehensive analysis for rotorcraft. I - Rotor model and wake analysis , 1981 .
[6] J. Grant,et al. The prediction of supercritical pressure distributions on blade tips , 1978 .
[7] Inderjit Chopra,et al. Effects of three-dimensional aerodynamics on blade response and loads , 1991 .
[8] Francis X. Caradonna,et al. Numerical Calculation of Unsteady Transonic Potential Flow over Helicopter Rotor Blades , 1975 .
[9] Wayne Johnson,et al. Correlation of Puma airloads: Lifting-line and wake calculation , 1989 .
[10] Roger C. Strawn,et al. Prediction of unsteady transonic rotor loads with a full-potential rotor code , 1987 .
[11] Roger C. Strawn,et al. Computational and experimental evaluation of helicopter rotor tips for high-speed flight , 1991 .