Bow Wave Effect in Aerial Refueling: Computational Analysis and Modeling-Reference-Cited by-同舟云学术

Bow Wave Effect in Aerial Refueling: Computational Analysis and Modeling

Published:2013-11 Issue:6 Volume:50 Page:1856-1868
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Dogan Atilla¹,Blake William²,Haag Christian²

Affiliation:

1. Department of Mechanical and Aerospace Engineering, University of Texas at Arlington, Arlington, Texas 76019

2. Aerospace Systems Directorate, U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032165

Reference27 articles.

1. Handling qualities design of the C-17A for receiver-refueling

2. Minimizing pilot-induced-oscillation susceptibility during C-17 development

3. HogansonE. H. “A Study of the Aerodynamic Interference Effects During Aerial Refueling,” M.S. Thesis, Air Force Inst. of Technology, School of Engineering, Wright–Patterson AFB, OH, Dec. 1983.

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