Review of cranked-arrow wing aerodynamics project: Its international aeronautical community role

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 9, Issue , 2007, Pages 5834-5865

  Lamar, John E ^a,b,c   Obara, Clifford J ^a,c,d  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Building 45   (United States)

^c AIAA   (United States)

^d MS 237   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERONAUTICAL COMMUNITY; FLIGHT CONDITIONS; FLIGHT DATASETS; SURFACE PRESSURES;

AERODYNAMICS; AEROSPACE ENGINEERING; BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; SKIN FRICTION; WIND TUNNELS;

WINGS;

EID: 34250861295     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (29)

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14. Lamar, John E.: Cranked Arrow Wing (F-16XL-1) Flight Flow Physics with CFD Predictions at Subsonic and Transonic Speeds. Presented at RIO AVT Symposium on Advanced Flow Management; Part A - Vortex Flow and High Angle of Attack, Paper Number 44, in Loen Norway during May 7-11, 2001.
15. Hummel, D. and Redeker, G.: A new vortex flow experiment for computer code validation. Presented at RTO AVT Symposium on Advanced Flow Management; Part A - Vortex Flow and High Angle of Attack, Paper Number 8, in Loen Norway during May 7-11, 2001.
16. Lamar, John E.; Conin, Catherine K.; and Scott, Laura E.: A Review of Steps Taken to Create an International Virtual Laboratory at NASA Langley for Aerodynamic Prediction and Comparison. Prog Aerospace Sci, Vol. 40, p. 163-172, 2004.
17. Lamar, John E.; Cronin, Catherine K.; and Scott, Laura E.: Virtual Laboratory Enabling Collaborative Research in Applied Vehicle Technologies. In AVT-123 Symposium on "Flow Induced Unsteady Loads and The Impact on Military Applications", Keynote 2, Budapest, Hungary, April 25-29, 2005.
18. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
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