An experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique

38th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2000, Pages

  Hwang, Danny P ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0346521059     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Bushnell, D.M. and Hrfner, J.N.: Viscous Drag Reduction in Boundary Layers. Progress in Astronautics and Aeronautics, volume 123. American Institute of Aeronautics and Astronautics. Inc. Washington. DC. 1990.
2. Jeromin, L.O.F.: An Experimental Investigation of the Compressible Turbulent Boundary Layer with Air Injection, ARC Reports and Memoranda No. 3526. Aeronautical Research Council, London. England, 1968.
3. Hrfner. J.N. and Bushnell. D.M.: Viscous Drag Reduction Via Surface Mass Injection. In V-e Reduction in Boundarv w. vol. 123. Progress in Astronauticsand Aeronautics, 1990.
4. Hwang, D.P.: A ProofofConcept Experiment for Reducing Skin Friction by Usinga Micro-Blowing Technique, AIAA-97-0546.
5. Hwang. D.P. a patent entitled: Skin Friction Reduction by Micro Blowing Technique, Patent no. 5.803.410. 1998.
6. Hwang, D.P. and Biesiadny, T.J.: Experimental Evaluation ofthe Penalty Associated With Micro-Blowing for Reducing Skin Friction, AIAA Paper AIAA-9X-0677.
7. Tillman, T.G.: Drag Reduction on a Large-Scale Nacelle Using Micro-Porous Blowing, United Technologies Research Center Report, R974.9 10.0001 1 December 1997.
8. Hwmg D.P.:SkinFrictionRcductionbyaMicro-BlowingTechnique. AIAA Journal. vol. 36, no. 3. pp. 480-481, March I998.
9. Tillman, T.G. and Hwang. D.P.: Drag Keduction on a Large-Scale Nacelle Using a Micro-Blowing Technique, AlAA Paper AIAA-99OI30.
10. Beltnn. L.R. Del Rosa. R.L. and Del Rosario. R.: Advanced Nozzle and Engine Componenls Test Facility, NASA TM-103684, 1992.
11. Ludwieg. H. andTillmann. W.: Investigationsofthe Wall Shearing Stress in Turbulent Boundary Layers, NACA Technical Memorandum 128.5. May 1950.