1 |
Nixon, D., 'Unsteady Transonic Aerodynamics', AIAA Progress in Astronautics and Aeronautics, Vol. 120, 1988
|
2 |
Murrnan, E. M., and Cole J. D., 'Calculation of Plane Study Transonic Flows', AIAA Journal, Vol. 9, N0.1, pp. 114-121, 1971
DOI
|
3 |
Hafes, E. M., South, J., and Murman, E., 'Artificial Compressibility Methods for Numerical Solutions of Transonic Full Potential Equation', AIAA Journal, Vol. 17, No.8, pp. 1737-1743, 1979
|
4 |
Roos, F. W. and Riddle, D. W., 'Measurements of Surface-Pressure and Wake-Flow Fluctuations in the Flow Field of a Whitcomb Supercritical Airfoil', NASA TN D-8443, 1977
|
5 |
Spaid, F. W., Dahlin, J. A, Roos, F. W., and Stivers, L. S., Jr., 'An Experimental Study of Transonic Flow about a Supercritical Airfoil. Static Pressure and Drag data Obtained from Tests of a Supercritical Airfoil and an NACA0012 Airfoil at Transonic Speeds, Supplement', NASA-TM-81336-SUPPL, 1983
|
6 |
Anderson, J. D. Jr., Introduction to Flight, 4th Ed., McGraw-Hill, pp. 227-344, 2000
|
7 |
Abbott, I. H. and von Doenhoff, A. E., Theory of Wing Sections, Dover Publications Inc. New York, 1959
|
8 |
Jameson, A. and Yoon, S., 'Multigrid Solution of the Euler Equations Using Implicit Schemes', AIAA Journal, Vol. 24, No. 11, pp.1737-1743, 1986
DOI
ScienceOn
|
9 |
Cole, J. D., Malmuth, N., and Wu, C. C., 'Transonic Wave Drag Estimation and Optimization Using the Nonlinear Area Rule'
|
10 |
Webster, B. E., Shephard, M. S., Rusak, Z., and Flaherty, J., 'An Automated Adaptive Time Discontinuous Finite Element Method for Unsteady Compressible Airfoil Aerodynamics', AIAA Journal, Vol. 32, No.4, pp. 748-757, 1994
DOI
ScienceOn
|
11 |
Cole, J. D. and Cook, L. P., Transonic Aerodynamics, North-Holland, 1986
|
12 |
Schwendenman, D. W., Kropinski, M. C. A, and Cole, J. D., 'On the Construction and Calculation of Optimal Nonlifting Critical Airfoils', Z. Angew. Math. Phys., Vol. 44, pp. 556-571, 1993
DOI
|
13 |
Whitcomb, R. T. and Clark, L. R, 'An Airfoil Shape for Efficient Flight at Supercritical Mach Numbers', NASA TM X-1109, 1965
|