Evaluation of Aerodynamic and Sonic Boom Performance of Supersonic Transport Aircrafts with Multiple Wing Configurations
In this study, two-dimensional airfoil shapes obtained in aerodynamic optimizations are converted to three-dimensional wing models and then their aerodynamic and sonic boom performance are evaluated. The airfoil shapes analyzed are the diamond, Busemann, new supersonic biplane (NSB), and triplane ai...
Saved in:
| Main Authors: | Wataru Yamazaki, Shu Ishida |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2025-05-01
|
| Series: | Aerospace |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/12/5/421 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Sonic Boom Impact Assessment of European SST Concept for Milan to New York Supersonic Flight
by: Giovanni Fasulo, et al.
Published: (2025-05-01) -
Numerical Simulation of Flapping Airfoil Aerodynamic Characteristics
by: Junjie Xu, et al.
Published: (2025-07-01) -
IMPROVING THE AERODYNAMICS OF A TRANSPORT AIRCRAFT WING USING A DELTA PLANFORM WINGTIP LEADING EDGE EXTENSION
by: D. Gueraiche, et al.
Published: (2018-03-01) -
A Numerical Approach for the Integration of Sonic Boom Requirements into the Matching Chart
by: Samuele Graziani, et al.
Published: (2025-06-01) -
Airfoil Preference and Adjustable Camber Impact Analysis for Trans-Medium Fixed-Wing Vehicles
by: Jixin LU, et al.
Published: (2025-02-01)