Double-decoupled inverse design of natural laminar flow nacelle under transonic conditions
Authors:
- Heng ZhangHZHeng Zhang
- Jie LiJLJie Li
- Zhao YangZYZhao Yang
Open Access
- 17 April 2023
- journal article
- research article
- Published by Elsevier in Chinese Journal of Aeronautics
- Vol. 36 (6) , 1-18
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China (12272312)
This publication has 27 references indexed in Scilit:
- Aerodynamic technologies to improve aircraft performanceAerospace Science and Technology, 2013
- Implementation of Menter's Transition Model on an Isolated Natural Laminar Flow NacelleAIAA Journal, 2011
- An inverse design method for engine nacelles and wingsAerospace Science and Technology, 2005
- Aerodynamic design of a natural laminar flow nacelle and the design validation by flight testingAerospace Science and Technology, 1998
- AIRCRAFT LAMINAR FLOW CONTROLAnnual Review of Fluid Mechanics, 1998
- Genetic optimization of target pressure distributions for inverse design methodsAIAA Journal, 1996
- Two-equation eddy-viscosity turbulence models for engineering applicationsAIAA Journal, 1994
- Aerodynamic shape design and optimization - Status and trendsJournal of Aircraft, 1992
- Feasibility study on the design of a laminar flow nacelleJournal of Aircraft, 1990
- Iterative three-dimensional transonic wing design using integral equationsJournal of Aircraft, 1985