Fast Aerodynamic Calculations Based on a Generalized Unsteady Coupling Algorithm-Reference-Cited by-同舟云学术

Fast Aerodynamic Calculations Based on a Generalized Unsteady Coupling Algorithm

Published:2021-05-10 Issue: Volume: Page:1-19
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Kharlamov Daniel¹,Da Ronch Andrea¹,Drofelnik Jernej¹,Walker Scott¹

Affiliation:

1. University of Southampton, Southampton, England SO17 1BJ, United Kingdom

Funder

Royal Academy of Engineering

Engineering and Physical Sciences Research Council

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference28 articles.

1. Transonic aeroelastic simulation for instability searches and uncertainty analysis

2. TaniI. “A Simple Method of Calculating the Induced Velocity of a Monoplane Wing,” Aeronautical Research Inst., Tokyo Imperial Univ. Rept. 111, Aug. 1934.

3. MulthoppH.SchwabeM., Die Berechnung der Auftriebsverteilung von Tragflügeln, Luftfahrt-Forschung, Vol. 15, April 1938, pp. 153–169.

4. SivellsJ. C.NeelyR. H. “Method for Calculating Wing Characteristics by Lifting-Line Theory Using Nonlinear Section Lift Data,” National Advisory Committee for Aeronautics, NACA-TN-1269, April 1947.

5. SivellsJ. C.WestrickG. C. “Method for Caluculating Lift Distributions for Unswept Wings with Flaps or Ailerons by Use of Nonlinear Section Lift Data,” National Advisory Committee for Aeronautics, NACA-TN-2283, 1951.

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