Evaluation of CFL3D for unsteady pressure and flutter predictions

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 7, Issue , 2003, Pages 4768-4777

  Hong, Moeljo S ^a   Kuruvila, Geojoe ^a   Bhatia, Kumar G ^a   SenGupta, Gautam ^a   Kim, Taehyoun ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; COMPUTATIONAL FLUID DYNAMICS; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; PRESSURE; STEADY FLOW; SUBSONIC FLOW; TRANSONIC FLOW; UNSTEADY FLOW;

FLIGHT VEHICLES; FLUTTER PREDICTION; REDUCED ORDER MODELING; UNSTEADY PRESSURE;

AEROSPACE ENGINEERING;

EID: 0042978734     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

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2. Silva, W. A., Bartels, R. E., "Development of Reduced-Order Models for Aeroelastic Analysis and Flutter Prediction Using the CFL3Dv6.0 Code", AIAA-2002-1596.
3. Kim, D. H., Park, Y. M., Lee, I., Kwon, O. J., "Nonlinear Aeroelastic Computation of Wings with Pylon/Finned-Store Using Parallel Unstructured Euler Solver", AIAA-2002-1289.
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8. Scott, R. C., Silva, W. A., Florence, J. R., Keller, D. F., "Measurement of Unsteady Pressure Data on a Large HSCT Semispan Wing and Comparison with Analysis", AIAA-2002-1648.
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10. Bartels, R. E., Biedron, R. T., "CFL3D version 6.0 User's Manual for Aeroelastic and Deforming Mesh Simulation"
11. Hong, M. S., "Evaluation of CFL3D for the Application of Fully Turbulent Airfoil", ER&D-BBA6-C2001-053, 2001 Boeing memo.
12. Kuruvila, G, "Evaluation and Enhancement of CFL3D for Aerodynamic and Aeroelastic Predictions", B-ADVTECH-LLL-M02-004, 2002 Lines Loads Laws Boeing memo.
13. Kim, T., "Frequency-Domain Karhunen-Loeve Method and Its Application to Linear Dynamic Systems," AIAA Journal, Vol. 36, No 11, pp. 2117-2123, Nov 1998.
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15. Kim, T., "Discrete-Time Eigen Analysis and Optimal Model Reduction for Flutter and Aeroelastic Damping/Frequency Prediction Based on CFL3D-ERA", B-ADVTECH-LLL-M02-13, 2002, Boeing memo.
16. Hong, M. S., "Evaluation of CFL3D for Steady Calibration Model and Wall Pressure Correlations in the Slotted Wall Transonic Dynamic Tunnel", B-ADVTECH-LLL-M02-005, 2002 Lines Loads Laws Boeing memo.