Cruise Drag Reduction Through Chord Modulation with Application to Distributed Propulsion-Reference-Cited by-同舟云学术

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Cruise Drag Reduction Through Chord Modulation with Application to Distributed Propulsion

Published:2022-09 Issue:5 Volume:59 Page:1112-1119
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Traub Lance W.¹

Affiliation:

1. Embry Riddle Aeronautical University, Prescott, Arizona 86301

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036612

Reference27 articles.

1. PrandtlL.BetzA., Vier Abhandlungen zur Hydrodynamik und Aerodynamik, Kaiser Wilhem Inst. for Flow Research, Göttingen, Germany, 1927, p. 31.

2. MunkM. “The Minimum Induced Drag of Airfoils,” NACA TR-121, 1921.

3. JonesR. T. “The Spanwise Distribution of Lift for Minimum Induced Drag of Wings Having a Given Lift and a Given Bending Moment,” NASA TN 2249, Dec. 1950.

4. Approximate solution of minimum induced drag of wings with given structural weight

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