Drag, lift, and moment estimates of transonic aircraft using the Navier-Stokes equations

AIAA Paper

Volumn , Issue , 2004, Pages 5368-5389

  Klausmeyer, Steven M ^a  

^a CESSNA AIRCRAFT COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL DERIVATIVES; PC-BASED COMPUTER CLUSTERS; REYNOLDS-AVERAGED NAVIER STOKES (RANS) METHODS; VISCOUS-DOMINATED STABILITY;

AEROSPACE INDUSTRY; AIRFOILS; BOUNDARY LAYER FLOW; CALIBRATION; COMPUTATIONAL FLUID DYNAMICS; DRAG; JET AIRCRAFT; LIFT; METHOD OF MOMENTS; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; ROBUSTNESS (CONTROL SYSTEMS); TRANSONIC AERODYNAMICS; TURBULENCE;

SUPERSONIC AIRCRAFT;

EID: 2942740905     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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3. Levy, D.W., et al, "Summary of Data from the First AIAA CFD Drag Prediction Workshop," AIAA-2002-0841.
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10. Laflin, K. R., et al., "Summary of Data from the Second AIAA CFD Drag Prediction Workshop," AIAA-2004-0555.
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12. Mavriplis, D. and Venkatakrishnan, V., "A unified multi-grid solver for the Navier-Stokes equations on mixed element meshes", International Journal for Computational Fluid Dynamics, 8:247-263, 1997.
13. Pfeiffer, Neal J., "Reflections on the Second Drag Prediction Workshop," AIAA-2004-0557.
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