Rapid technology focused experimental and computational aerodynamic investigation of a strike tanker

USAF Developmental Test and Evaluation Summit

Volumn , Issue , 2004, Pages

  Tyler, Charles ^a   Reeder, Mark F ^b   Braisted, William ^c   Higgins, James ^c   Gebbie, Lt David ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^c UNIVERSITY OF DAYTON RESEARCH INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR FORCE INSTITUTE OF TECHNOLOGIES; AIR FORCE RESEARCH LABORATORY; COMPUTATIONAL FLUID DYNAMICS ANALYSIS; COMPUTATIONAL RESULTS; LOW-SPEED WIND TUNNEL; SURFACE PRESSURE MEASUREMENTS; UNIVERSITY OF DAYTON; WIND-TUNNEL TESTING;

ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; AUTOMOBILE MANUFACTURE; COMPUTATIONAL FLUID DYNAMICS; DESIGN; TESTING;

WIND TUNNELS;

EID: 84896692774     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Tyler, C., Braisted, W., Higgins, J., "Evaluation of Rapid Prototyping Technologies for Use in Wind Tunnel Model Fabrication," AIAA Paper 2005-1301.
2. Liebeck, R.H., "Blended Wing Body Design Challenges", AIAA Paper 2003-2659.
3. Liebeck, "Design of the Blended Wing Body Subsonic Transport," AIAA Journal of Aircraft, Vol. 41, No. 1, pp. 10-25, Jan. 2004.
4. Katz, J., Byrne, S. & Hahl, R. "Stall Resistance Features of Lifting-Body Airplane Configurations," AIAA Journal of Aircraft, Vol. 26, No. 2, pp. 471-474, 1999.
5. Carlsson, M. & Kuttenkeuler, J. "Design and Testing of a Blended Wing Body Aeroelastic Wind-Tunnel Model," AIAA Journal of Aircraft, Vol. 40, No. 1, pp. 211-213, 2003.
6. rd edition, Wiley and Sons, 1999.
7. Hemsch, M., "Statistical Analysis of Computational Fluid Dynamics Solutions from the Drag Prediction Workshop," AIAA Journal of Aircraft, Vol. 41, No. 1, pp. 95-103, Jan. 2004.