Wind tunnel investigation of the transonic aerodynamic characteristics of forward swept wings
Author:
Affiliation:
1. Air Force Wright Aeronautical Laboratories, Wright-Patterson Air Force Base, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44853
Reference3 articles.
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1. Lift and Tip Vortices Generated by Tapered Backward-Swept and Forward-Swept Wings under Stationary Ground Proximity;Journal of Aerospace Engineering;2023-09
2. Supersonic Forward-Swept Wing Design Using Multifidelity Efficient Global Optimization;Journal of Aircraft;2022-07
3. Elements of Aerodynamic Wing Design;Advanced Aircraft Design;2013-05-27
4. Hybridizing Genetic Algorithm with Artificial Neural Network in the Aerodynamic Optimization of the Forward Swept Wing;51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th;2010-04-12
5. Aerodynamic Characteristics of Forward and Aft Swept Arrow Wings;Journal of Aircraft;2009-07
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