Transonic Wing Design Using Inverse and Optimization Methods
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 soph...
Main Authors: | A. L. Bolsunovsky, N. P. Buzoverya |
---|---|
Format: | Article |
Language: | English |
Published: |
CTU Central Library
2000-01-01
|
Series: | Acta Polytechnica |
Online Access: | https://ojs.cvut.cz/ojs/index.php/ap/article/view/8 |
Similar Items
-
Optimization Procedure for Design of High-lift Airfoils with Specified Stall Behaviour
by: A. L. Bolsunovsky, et al.
Published: (2000-01-01) -
Aerostructural Design Exploration of a Wing in Transonic Flow
by: Nicolas P. Bons, et al.
Published: (2020-08-01) -
Aerodynamic inverse design of transonic turbomachinery cascades
by: Ahmadi, Majid
Published: (1998) -
Inverse Design of Airfoil using Elastic Surface Method in Viscous Subsonic and Transonic Flow
by: M. Safari, et al.
Published: (2015-07-01) -
Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft
by: Meadows, Nicholas Andrew
Published: (2014)