Wake integration method for airfoil drag evaluation using N-S equations

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

Volumn 32, Issue 3, 2006, Pages 288-292

  Liu, Zhou ^a   Zhu, Ziqiang ^a   Wang, Xiaolu ^a   Wu, Zongcheng ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Drag evaluation; N S equations; Surface integration; Wake integration

Indexed keywords

DRAG; EVALUATION; INTEGRATION; THREE DIMENSIONAL; WAKES;

DRAG EVALUATION; N S EQUATIONS; SURFACE INTEGRATION; THREE DIMENSIONAL CONFIGURATIONS; WAKE INTEGRATION;

AIRFOILS;

EID: 33745153422     PISSN: 10015965     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (13)

1. Paterson J H, Blackerby W T, Schwanebeck J C. Analysis of flight test data on the C-141A aircraft[R]. NASA CR-1558, Washington, D C: NASA, 1970
2. MacWilkinson D G, Blackerby W T, Paterson J H. Correlation of full-scale drag predictions with flight measurements on the C-141A aircraft-phase II, wind tunnel test, analysis, and prediction techniques[R]. NASA CR-2333, Washington, D C: NASA, 1974
3. Meredith P T. Viscous phenomena affecting high-lift systems and suggestions for future CFD development[A]. High-Lift Systems Aerodynamics, AGARD CP 315[C]. London: Technical Editing and Reproduction, Ltd, 1993
4. Liu Zhou, Zhu Ziqiang, Fu Hongyan, et al. Design of airfoil with high ratio of lift over drag[J]. Acta Aerodynamica Sinica, 2004, 22(4): 410-415(in Chinese)
5. Tinoco E N. An assessment of CFD prediction of drag and other longitudinal characteristics[R]. AIAA 2001-1002, 2001
6. Peavey C C. Drag prediction for military aircraft using CFD[R], AIAA 2000-0383, 2000
7. Van Dam C P. Recent experience with different methods of drag prediction[J]. Progress in Aerospace Sciences, 1999, 35: 751-798
8. Van Dam C P, Nikfetrat K, Wong K. Drag prediction at subsonic and transonic speeds using Euler methods[J]. Journal of Aircraft, 1995, 32(4): 839-845
9. Liu Jie, Zhu Ziqiang, Chen Zemin, et al. Wake integration method for aerodynamics evaluation using Euler equations[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(4): 417-42l(in Chinese)
10. Chao D D, Van Dam C P. Airfoil drag prediction and decomposition[R]. AIAA, 98-2783, 1998
11. Jameson A, Schmidt W, Turkel E. Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes[R]. AIAA 81-1259, 1981
12. Baldwin B S, Lomax H. Thin layer approximation and algebraic model for separated turbulent flows[R]. AIAA 78-257, 1978
13. Cook P H, McDonald M A, Firmin M C P. Aerofoil RAE2822-pressure distributions, and boundary layer and wake measurements[R]. AGARD-AR-138, 1979