Study of semi-Span model testing techniques

14th Applied Aerodynamics Conference

Volumn , Issue , 1996, Pages 130-146

  Gatlin, Gregory M ^a   McGhee, Robert J ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYER FLOW; ENERGY EFFICIENCY; FLOORS; FUSELAGES; LIFT; NASA; TESTING; WIND TUNNELS;

BOUNDARY LAYER HEIGHTS; BOUNDARY LAYER MEASUREMENTS; BOUNDARY-LAYER CONTROL; MAXIMUM LIFT COEFFICIENT; SPAN CONFIGURATION; STAND OFF HEIGHT; SURFACE PRESSURES; TANGENTIAL BLOWING;

BOUNDARY LAYERS;

EID: 84964260965     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. Lynch, F. T.: Experimental Necessities for Subsonic Transport Configuration Development. AIAA Paper 92-0158, January 1992.
2. Viehweger, G.; and Ewald, B.: Half Model Testing in the Cologne Cryogenic Tunnel (KKK). AIAA Paper 94-25 11, June 1994.
3. Milholen, W. E.; and Chokani, N.: Effect of Sidewall Boundary Layer on Transonic Flow Over a Wing. Journal of Aircraft, Vol. 31, July 1994, pp. 986-988.
4. Franz, H. P.: The Half-Model Technique in the Wind Tunnel and its Employment in the Development of the Airbus Family. NASA TM-76970, August 1982. Translation of DGLR Paper 81-118.
5. Boersen, S. J.: Half-Model Testing in the NLR High-speed Wind Tunnel HST, A 1981 Status Report. NLR TR 82123U, August 1982.
6. Earnshaw, P. B.; Green, A. R.; Hardy, B. C.; and Jelly, A. H.: A Study of the use of Half-Models in High-Lift Wind-Tunnel Testing. AGARD-CP-515, October 1992, pp. 20.1-20.9.
7. Milholen W. E.; Chokani, N.; and McGhee, R. J.: Development of Semi-span Model Test Techniques. AIAA Paper 96-2412, June 1996.
8. Gentry, Garl L.; Quinto, P. Frank; Gatlin, Gregory M.; and Applin, Zachary T.: The Langley 14- by 22-Foot Subsonic Tunnel: Description, Flow Characteristics, and Guide for Users. NASA TP-3008, September 1990.
9. Paschal, K., Goodman, W., McGhee, R., Walker, B., and Wilcox, P. A.: Evaluation of Tunnel Sidewall Boundary-Layer-Control Systems for High-Lift Airfoil Testing. AIAA Paper 91-3243, September 1991.