Development of two-element NLF airfoils for long endurance flight

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Koss, D ^a   Steinbuch, M ^a   Shepshelovich, M ^a  

^a ISRAEL AIRCRAFT INDUSTRIES   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; AIRFOILS; ASPECT RATIO;

ENDURANCE AIRCRAFT; EXPERIMENTAL EVALUATION; HIGH LIFTS; HIGH-ASPECT RATIO WING; HINGE MOMENT; INTERNAL VOLUME; THICKNESS RATIO; VARIABLE GEOMETRY;

FLIGHT ENVELOPES;

EID: 84982318631     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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2. Liebeck, R. H., "Design of Subsonic Airfoils for High Lift", AIAA Paper 76-406, AIAA 9th Fluid and Plasma Dynamics Conference, S. Diego, July 1976.
3. Koss, D. and Shepshelovich, M., "Design and Experimental Evaluation of a Two-Element, High-Lift / Low-Drag, Long-Endurance Airfoil", Proc. of the 35th Israel Annual Conference on Aerospace Sciences, Israel, Feb. 1995.
4. Drela, M. and Giles, M. B., "Viscous-Inviscid Analysis of Transonic and Low Reynolds Number Airfoils", AIAA Journal, 25 (10), Oct. 1987.
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9. Liebeck, R. H., "Low Reynolds Number Airfoil Design for Subsonic Compressible Flow", Douglas Paper 8274, Conference on Low Reynolds Number Aerodynamics, Univ. of Notre Dame, June 1989.
10. Reuther, J., Van Dam, C. and Hicks, R., "Subsonic and Transonic Low Reynolds Number Airfoils with Reduced Pitching Moment", AIAA 90-3212, AIAA/AHS/ASEE Aircraft Design, Systems and Operations Conference, Sept. 1990.
11. Drela, M., "Transonic Low Reynolds Number Airfoils", AIAA 91-3337, 9th AIAA Applied Aerodynamics Conference, Sept. 1991.
12. Steinbuch, M., Koss, D. and Shepshelovich, M., "Wing Development for High Altitude, Long Endurance Flight", Proc. of the 35th Israel Annual Conference on Aerospace Sciences, Feb. 1995.
13. Steinbuch, M., Shepshelovich, M. and Tumin, A., "Laminarization of the Swept Wing-The Design Aspects", Proc. of the 36th Israel Annual Conference on Aerospace Sciences, Feb. 1996.
14. Liebeck, R. H. and Camacho, P.P., "Airfoil Design at Low Reynolds Number with Constrained Pitching Moment", UNDAS CP-77B123, Proc. of the Conference on Low Reynolds Number Aerodynamics, June 1985.