Unsteady transonic algorithm improvements for realistic aircraft applications

Journal of Aircraft

Volumn 26, Issue 2, 1989, Pages 131-139

  Batina, John T ^a,b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Structural Dynamics Division ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT, MILITARY--WINGS; MATHEMATICAL TECHNIQUES--FINITE DIFFERENCE METHOD;

AEROELASTIC PHENOMENA; APPROXIMATE FACTORIZATION ALGORITHM; COMPUTER CODE CAP-TSD; SOFTWARE PACKAGE CAP-TSD; TRANSONIC SMALL DISTURBANCE EQUATION;

AERODYNAMICS;

EID: 0024606453     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.45734     Document Type: Article

References (16)

1. 'Edwards, J. W. and Thomas, J. L., "Computational Methods for Unsteady Transonic Flows," AIAA Paper 87-0107, Jan. 1987.
2. Batina, J. T., Seidel, D. A., Bland, S. R., and Bennett, R. M., "Unsteady Transonic Flow Calculations for Realistic Aircraft Configurations," AIAA Paper 87-0850, April 1987.
3. Cunningham, H. J., Batina, J. T., and Bennett, R. M., "Modern Wing Flutter Analysis by Computational Fluid Dynamics Methods," ASME Winter Annual Meeting, Boston, MA, Dec. 1987.
4. Batina, J. T., "An Efficient Algorithm for Solution of the Unsteady Transonic Small-Disturbance Equation," AIAA Paper 87-0109, Jan. 1987.
5. Murman, E. M., "Analysis of Embedded Shock Waves Calculated by Relaxation Methods," Proceedings of AIAA Computational Fluid Dynamics Conference, AIAA, New York, 1973, pp. 27-40.
6. Engquist, B. E. and Osher, S. J., "Stable and Entropy Satisfying Approximations for Transonic Flow Calculations," Mathematics of Computation, Vol. 34, No. 149, Jan. 1980, pp. 45-75.
7. Goorjian, P. M., Meagher, M. E., and Van Buskirk, R., "Monotone Implicit Algorithms for the Small-Disturbance and Full Potential Equations Applied to Transonic Flows," AIAA Paper 83-0371, Jan. 1983.
8. Goorjian, P. M. and Van Buskirk, R. D., "Second-Order-Accurate Spatial Differencing for the Transonic Small-Disturbance Equation," Journal of Aircraft, Vol. 23, Nov. 1985, pp. 1693-1699.
9. Whitlow, W., Jr., "Characteristic Boundary Conditions for Three-Dimensional Transonic Unsteady Aerodynamics," NASA TM-86292, Oct. 1984.
10. Tijdeman, H., Van Nunen, J. W. G., Kraan, A. N., Persoon, A. J., Poestkoke, R., Roos, R., Schippers, P., and Siebert, C. M., "Transonic Wind Tunnel Tests on an Oscillating Wing with External Stores," AFFDL-TR-78-194, Air Force Flight Dynamics Lab., Dayton, OH, Dec. 1978.
11. Schmitt, V. and Charpin, F., "Pressure Distributions on the ONERA M6 Wing at Transonic Mach Numbers," Experimental Data Base for Computer Program Assessment, AGARD-AR-138, Appendix Bl, May 1979.
12. Fox, M. C. and Feldman, C. S., "Model and Test Information Report, 1/9-Scale F-16C and F-16D Force and Loads Model," General Dynamics Rept. 16PR2179, Jan. 1982.
13. Feldman, C. S., "Wind Tunnel Data Report, 1/9-Scale F-16C Pressure Loads Test," General Dynamics Rept. 16PR2252, July 1982.
14. Bland, S. R., "Development of Low-Frequency Kernel-Function Aerodynamics for Comparison with Time-Dependent Finite-Difference Methods," NASA TM-83283, May 1982.
15. Seidel, D. A., Bennett, R. M., and Whitlow, W., Jr., "An Exploratory Study of Finite Difference Grids for Transonic Unsteady Aerodynamics," NASA TM-84583, Dec. 1982.
16. Batina, J. T., "Unsteady Transonic Algorithm Improvements for Realistic Aircraft Applications," AIAA Paper 88-0105, Jan. 1988.