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Prediction and Experimental Evaluation of Planar Wing Spanloads for Minimum Drag

  • Published:2017-09 Issue:5 Volume:54 Page:1664-1674
  • ISSN:0021-8669
  • Container-title:Journal of Aircraft
  • language:en
  • Short-container-title:Journal of Aircraft

Author:

Wroblewski Gabrielle E.1,Ansell Phillip J.1

Affiliation:

1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801

Funder

National Aeronautics and Space Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference38 articles.

1. PrandtlL. “Applications of Modern Hydrodynamics to Aeronautics,” NACA TR-116, 1923.

2. MunkM. M. “The Minimum Induced Drag of Aerofoils,” NACA TR-121, 1923.

3. ConeC. D. “The Theory of Induced Lift and Minimum Induced Drag of Nonplanar Lifting Systems,” NASA TR-139, 1962.

4. DeYoungJ. “Induced Drag Ideal Efficiency Factor of Arbitrary Lateral-Vertical Wing Forms,” NASA CR 3357, 1980.

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