Low reynolds number testing of the AG38 airfoil for the SAMARAI nano air vehicle

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Youngren, Harold ^a   Kroninger, Chris ^b   Chang, Ming ^c   Jameson, Steve ^c  

^a AeroCraft Consulting   (United States)

^b U S ARMY RESEARCH LABORATORY   (United States)

^c LOCKHEED MARTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR VEHICLE; COMPUTATIONAL RESULTS; DEFENSE ADVANCED RESEARCH PROJECTS AGENCIES; EXPERIMENTAL AERODYNAMICS; EXPERIMENTAL DATA; EXPERIMENTAL MODELS; FIXED WING; FLAPPING WING; FLYING VEHICLES; GOOD CORRELATIONS; LAMINAR SEPARATION BUBBLE; LOCKHEED MARTIN; LOW REYNOLDS NUMBER; NON-LINEAR; ROTARY WING; SCALE SIZES; TOTAL MASS; TURBULATORS;

AERODYNAMICS; AEROSPACE ENGINEERING; AIRFOILS; FIXED WINGS; LAMINAR FLOW; REYNOLDS NUMBER;

VEHICLES;

EID: 78149432054     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

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2. Selig, M.S., Guglielmo, J.J., Broeren, A.P., and Gigùere, P., Summary of Low-Speed Airfoil Data - Vol. 1, SoarTech Publications, Virginia Beach, VA, 1995.
3. Selig, M.S., Lyon, C.A., Gigùere, P., Ninham, C.P., and Guglielmo, J.J., Summary of Low-Speed Airfoil Data - Vol. 2, SoarTech Publications, Virginia Beach, VA, 1996.
4. Lyon, C.A., Broeren, A.P., Gigùere, P., Gopalarathnam, A., and Selig, M.S., Summary of Low-Speed Airfoil Data - Vol. 3, SoarTech Publications, Virginia Beach, VA, 1997.
5. Michael S. Selig and Bryan D. McGranahan, Wind Tunnel Aerodynamic Tests of Six Airfoils for Use on Small Wind Turbines, NREL/SR-500-34515, University of Illinois at Urbana-Champaign, January 31, 2003.
6. McGhee, R.J., Walker, B.S., and Millard, B.F., "Experimental Results for the Eppler 387 Airfoil at Low Reynolds Numbers in the Langley Low-Turbulence Pressure Tunnel, " NASA TM 4062, October 1988.
7. Receptivity and Growth of Two- and Three-Dimensional Disturbances in a Blasius Boundary Layer, Rudolph A. King, MIT Aeronautics and Astronautics PhD Thesis, February 11, 2000.
8. XFOIL, description and methodology discussed in: Low Reynolds Number Aerodynamics, T.J. Mueller (Editor), Lecture Notes in Engineering #54, Springer Verlag. 1989. ISBN 3-540-51884-3, ISBN 0-387-51884-3.
9. Rae, W.H., and Pope, A., Low Speed Wind Tunnel Testing, Second Edition, John Wiley and Sons, Inc., 1984.