Response Surface Method for Airfoil Design in Transonic Flow

By Jaekwon Ahn, H. Kim, Dong-Ho Lee, O. Rho. 2001

52 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/e49f96fcd83f25b970f0c3427347acb0bcce397d

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Ning Qin
2. A. Vavalle

In Computational Mechanics

1. Ning Qin
2. A. Vavalle
3. Christian B. Allen
4. Thomas C. S. Rendall

Citations in the corpus

• Iterative Response Surface Based Optimization Scheme for Transonic Airfoil Design (2007, methodology): “The preferred method to sample the design space in aerodynamic optimization [2,15] has been to compute the test matrix to satisfy the D-optimality criterion These designs of experiments maximize the determinant of the least-square matrix.”