Prediction of F-16XL flight-flow physics

Journal of Aircraft

Volumn 46, Issue 2, 2009, Pages 354-

  Lamar, John E ^a,b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b AVT 113 ^*

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; DELTA WING AIRCRAFT; RESEARCH AIRCRAFT; WINGS;

APPLIED VEHICLE TECHNOLOGIES; CRANKED-ARROW WING; DELTA WING MODEL; FRICTION MEASUREMENTS; GOVERNMENT LABORATORIES; INTERNATIONAL COMPARISON; INTERNATIONAL GROUP; VORTICAL FLOWS;

SUPERSONIC AIRCRAFT;

EID: 63349110310     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.35182     Document Type: Article

References (2)

1. Lamar, J.E., Obara, C.J., Fisher, B. D., and Fisher, D.F.,"Flight, Wind-Tunnel, and a Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds," NASA TP-2001-210629, Feb. 2001.
2. Hummel, D., and Redeker, G., "A New Vortex Flow Experiment for Computer Code Validation," RTOAVT Symposium on Advanced Flow Management; Part A - Vortex Flow and High Angle of Attack, Paper 8, 7-11 May 2001.