33 results on '"Hicks R"'
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2. Practical design optimization of wing/body configurations using the Euler equations
3. Subsonic and transonic low-Reynolds-number airfoils with reduced pitching moments
4. Euler and Potential Experiment/CFD Correlations for a Transport and Two Delta-Wing Configurations
5. Euler and potential computational results for selected aerodynamic configurations
6. An evaluation of three helicopter rotor sections
7. A recontoured, upper surface designed to increase the maximum lift coefficient of a modified NACA 65 (0.82) (9.9) airfoil section
8. An assessment of a modified potential flow code for calculating the effect of small geometric change on the pressure and forces of supercritical airfoils
9. Transonic wing design using potential-flow codes - Successes and failures
10. An evaluation of the method for determining the Whitham F-function using distributions of downwash and sidewash angles
11. Airfoil section drag reduction at transonic speeds by numerical optimization
12. Effects of forward contour modification on the aerodynamic characteristics of the NACA 641-212 airfoil section
13. Design of low-speed airfoils by numerical optimization
14. Application of numerical optimization to the design of low speed airfoils
15. An assessment of airfoil design by numerical optimization
16. An experimental evaluation of a helicopter rotor section designed by numerical optimization
17. Computerized three-dimensional aerodynamic design of a lifting rotor blade
18. Upper-surface modifications for C sub l max improvement of selected NASA 6-series airfoils
19. Effects of upper surface modification on the aerodynamic characteristics of the NACA 63 sub 2-215 airfoil section
20. Computational optimization and wind tunnel test of transonic wing designs
21. Supercritical wing design using numerical optimization and comparisons with experiment
22. Application of numerical optimization to the design of advanced supercritical airfoils
23. Airfoil design by numerical optimization using a minicomputer
24. Wing analysis using a transonic potential flow computational method
25. Transonic wing analysis using advanced computational methods
26. Wing design by numerical optimization
27. Application of numerical optimization to the design of supercritical airfoils without drag-creep
28. Numerical Airfoil Optimization Using a Reduced Number of Design Coordinates
29. Airfoil section drag reduction at transonic speeds by numerical optimization
30. Measurements of local skin friction downstream of grit-type boundary-layer-transition trips at M equals 2.17 and zero heat transfer
31. Some effects of Mach number and geometry on sonic boom
32. Aerodynamic characteristics of several cranked leading-edge wing-body combinations at Mach numbers from 0.4 to 2.94
33. Use of grit-type boundary-layer transition trips on wind-tunnel models
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