Transonic Wing Design Using Inverse and Optimization Methods

Authors

  • A. L. Bolsunovsky
  • N. P. Buzoverya

DOI:

https://doi.org/10.14311/8

Abstract

Presented is an effective procedure for aerodynamic design of transonic wings, based on joint use of fast method for direct calculation and inverse and numerical optimization methods developed by the authors. Each component of the procedure developed is described. Some examples of designing sophisticated advanced configurations are given.

Downloads

Author Biographies

  • A. L. Bolsunovsky
  • N. P. Buzoverya

Published

2000-01-01

Issue

Vol. 40 No. 1 (2000)

Section

Articles

License

Copyright (c) 2015 Acta Polytechnica

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

Bolsunovsky, A. L., & Buzoverya, N. P. (2000). Transonic Wing Design Using Inverse and Optimization Methods. Acta Polytechnica, 40(1). https://doi.org/10.14311/8