High fidelity methods and physics for UAV flow regimes

Proceedings - Department of Defense High Performance Computing Modernization Program Users Group Conference, UGC 2004

Volumn , Issue , 2004, Pages 138-143

  Melville, Reid ^a   Visbal, Miguel ^a   Gordnier, Raymond ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; COMPUTATIONAL METHODS; COMPUTER SIMULATION; ELASTICITY; NONLINEAR CONTROL SYSTEMS; PROBLEM SOLVING; SENSITIVITY ANALYSIS;

HIGH FIDELITY METHODS; LARGE-EDDY SIMULATION (LES); NONLINEAR FLOW; UNAMMANED AERIAL VEHICLES (UAV);

UNMANNED VEHICLES;

EID: 21444433776     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/dod_ugc.2004.21     Document Type: Conference Paper

References (13)

1. Morgan, P. and M. Visbal, "Large-Eddy Simulation of Airfoil Flows." AIAA Paper 2003-0777, January 2003.
2. Morgan, P. and M. Visbal, "Large-Eddy Simulation Modeling Issues for Flow Around Wing Sections." AIAA Paper 2003-4152, June 2003.
3. Sherer, S., "Further Analysis of High-Order Overset Grid Method with Applications." AIAA Paper 2003-3839, Orlando, FL, June 2003.
4. Sherer, S., "Direct Numerical and Large-Eddy Simulations Using a High-Order Overset Grid Solver." AIAA Paper 2004-2530, Portland, OR, June 2004.
5. Rizzetta, D.P. and M.R. Visbal, "Numerical Investigation of Transitional Flow through a Low-Pressure Turbine Cascade." AIAA Paper 2003-3587, June 2003.
6. Rizzetta, D.P. and M.R. Visbal, "Numerical Simulation of Separation Control for a Transitional Highly-Loaded Low-Pressure Turbine." AIAA Paper 2004-2204, June 2004.
7. Visbal, M.R., "Computational and Physical Aspects of Vortex Breakdown on Delta Wings." AIAA-95-0585, January 1995.
8. Rockwell, D., "Three-Dimensional Flow Structure on Delta Wings at High Angle-of-Attack: Experimental Concepts and Issues." AIAA-93-0550, January 1993.
9. Ol, M.V. and M. Gharib, "The Passage Toward Stall of Nonslender Delta Wings at Low Reynolds Number." AIAA-2001-2843, June 2001.
10. Taylor, G.S., T. Schnorbus, and I. Gursul, "An Investigation of Vortex Flows over Low Sweep Delta Wings." AIAA-2003-4021, June 2003.
11. Gordnier, R.E. and M.R. Visbai, "Higher-Order Compact Difference Scheme Applied to the Simulation of a Low Sweep Delta Wing Flow." AIAA-2003-0620, January 2003.
12. Taylor, G.S. and I. Gursul, "Lift Enhancement over a Flexible Delta Wing." AIAA-2004-2618, June 2004.
13. Gordnier, R.E. and M.R. Visbal, "Numerical Simulation of Nonslender Delta Wing Buffet at High Angle-of-Attack." AIAA-2004-2047, April 2004.