Wake integration method for aerodynamics evaluation using Euler equations

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 26, Issue 4, 2005, Pages 417-421

  Liu, Jie ^a   Zhu, Zi Qiang ^a   Chen, Ze Min ^a   Wu, Zong Cheng ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Aerodynamics evaluation; Drag decomposition; Surface integration; Wake integration

Indexed keywords

AIRCRAFT; DECOMPOSITION; EQUATIONS OF MOTION; EVALUATION; INTEGRATION; STRUCTURAL DESIGN; WAKES; WINGS;

AERODYNAMICS EVALUATION; DRAG DECOMPOSITION; EULER EQUATIONS; FLOW FIELD; SURFACE INTEGRATION; WAKE INTEGRATION;

AERODYNAMICS;

EID: 23944449907     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)

1. van Dam C P, Nikfetrat K, Accurate prediction of drag using Euler methods[J]. Journal of Aircraft, 1992, 29(3): 516-519.
2. Chao D D, van Dam C P. Airfoil prediction and decomposition[R]. AIAA Paper 98-2783, 1998.
3. van Dam C P, Nikfetrat K. Drag prediction at subsonic and transonic speeds using Euler methods[J]. Journal of Aircraft, 1995, 32(4): 839-845.
4. Cummings R M, Giles M B, Shrinivas G N. Analysis of the elements of drag in three-dimensional viscous and inviscid flows[R]. AIAA Paper 96-2482, 1996.
5. Hunt D L, Cummings R M, Giles M B. Determination of drag from three-dimensional viscous and inviscid flowfield computation[R]. AIAA Paper 97-2257, 1997.