Local Piston Theory as an Alternative to Mesh Deformation: Slender Wing/Body Configurations
Author:
Affiliation:
1. University of Pretoria, Pretoria 0081, South Africa
2. Northumbria University, Newcastle upon Tyne, England NE1 8ST, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034697
Reference34 articles.
1. YatesE.BlandS. “Comparative Evaluation of Methods for Predicting Flutter and Divergence of Unswept Wings of Finite Span,” NASA TN D-2051, 1963.
2. AndersonJ., Fundamentals of Aerodynamics, 3rd ed., McGraw–Hill Education, New York, 2001, pp. 391–398.
3. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.
4. Constant pressure panel method for supersonic unsteady airload analysis
5. Supersonic Flutter Analysis Based on a Local Piston Theory
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