Amanote Research
Register
Sign In
Supersonic Inverse Design Method for Wing-Fuselage Design
doi 10.1016/b978-008043319-6/50044-3
Full Text
Open PDF
Abstract
Available in
full text
Date
January 1, 1998
Authors
Shinkyu Jeong
Shigeru Obayashi
Kazuhiro Nakahashi
Toshiyuki Iwamiya
Kisa Matsushima
Publisher
Elsevier
Related search
Hybrid Wing Body Pressurized Fuselage and Bulkhead Design and Optimization
On the Use of Direct and Inverse Numerical Flow Calculations for Supersonic Turbine Design
Adjoint-Based Method for Supersonic Aircraft Design Using Equivalent Area Distribution
Wing Mass Formula for Twin Fuselage Aircraft
Journal of Aircraft
Aerospace Engineering
Inviscid-Viscous Interaction Method for 3D Inverse Design of Centrifugal Impellers
Inverse Design Tool for Ion Optical Devices Using the Adjoint Variable Method
Scientific Reports
Multidisciplinary
An Inverse Approach for Airfoil Design
Inverse Airfoil Design Method for Low-Speed Straight-Bladed Darrieus-Type VAWT Applications
Wind Engineering
Renewable Energy
Power Technology
the Environment
Sustainability
Energy Engineering
Multimodality in Aerodynamic Wing Design Optimization
AIAA Journal
Aerospace Engineering