Wing Tip Vortices from an Exergy-Based Perspective
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of Dayton, Dayton, Ohio 45469
2. Institute of Aerospace Systems (ILR), RWTH Aachen University, 52062 Aachen, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032854
Reference16 articles.
1. Aerodynamik des Flugzeuges
2. Wake vortex characteristics of transport aircraft
3. Benefits of Exergy-Based Analysis for Aerospace Engineering Applications: Part 1
4. FigliolaR.TiptonR. “An Exergy-Based Methodology for Decision-Based Design of Integrated Aircraft Thermal Systems,” Soc. of Automotive Engineers TP-2000-01-5527, Warrendale, PA, 2000.
5. Nature of Wakelike and Jetlike Axial Tip Vortex Flows
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2. Wingtip vortex structure in the near-field of swept-tapered wings;Physics of Fluids;2020-09-01
3. Adopting exergy analysis for use in aerospace;Progress in Aerospace Sciences;2017-08
4. Cross-stream Contributions to Wing Wake Free Shear Layers Using Particle Image Velocimetry: Challenges and Results;55th AIAA Aerospace Sciences Meeting;2017-01-05
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