Aerodynamic anomalies - Can CFD prevent or correct them?

作者: Richard S. Shevell

DOI: 10.2514/3.45356

关键词: AerodynamicsEngineeringComputational fluid dynamicsDragPerformance predictionDesign toolFlight testAerospace engineeringMechanical engineeringWingAirfoil

摘要: Computational fluid dynamics (CFD) has become a standard design tool for modern sophisticated aircraft. This paper reviews methods that were used some existing jet transport aircraft at time when theoretical tools had very limited capability. Early designers combined available theory and empirical data with sufficient skill to develop highly successful They also overcome serious problems sometimes arose only after first flight, due aerodynamic phenomena not predicted. Some of these are discussed in detail this paper. The questions whether CFD would have warned provided necessary solutions is addressed. It concluded that, many cases, the answer negative. Comparisons between two-dimensional airfoil compressibility drag rise, converted finite wing rise using simple sweep theory, flight test results show good agreement. A rapid method compressibili ty prediction based On suggested. will define can be expected if do proper job, thereby allowing early performance prediction. Actual task three-dimensional body code including viscous shock wave effects.

参考文章(7)
H.H. PEARCEY, THE AERODYNAMIC DESIGN OF SECTION SHAPES FOR SWEPT WINGS Advances in Aeronautical Sciences#R##N#Proceedings of the Second International Congress in the Aeronautical Sciences, Zürich, 12–16 September 1960. pp. 277- 322 ,(1962) , 10.1016/B978-0-08-006550-2.50021-1
RICHARD S. SHEVELL, Operational Aerodynamics of High-Speed Transport Aircraft Journal of the Aeronautical Sciences. ,vol. 15, pp. 133- 143 ,(1948) , 10.2514/8.11528
RICHARD S. SHEVELL, ROGER D. SCHAUFELE, Aerodynamic design features of the DC-9. Journal of Aircraft. ,vol. 3, pp. 515- 523 ,(1966) , 10.2514/3.43770
A. M. O. Smith, High-Lift Aerodynamics Journal of Aircraft. ,vol. 12, pp. 501- 530 ,(1975) , 10.2514/3.59830
Robert H. Korkegi, Impact of computational fluid dynamics on development test facilities Journal of Aircraft. ,vol. 22, pp. 182- 187 ,(1985) , 10.2514/3.45105
Luis R. Miranda, Application of computational aerodynamics to airplane design Journal of Aircraft. ,vol. 21, pp. 355- 370 ,(1984) , 10.2514/3.44974