Inverse design method on scramjet nozzles based on maximum thrust theory
Artificial neural network based inverse design: Airfoils and wings
An inverse design method for rail grinding profiles
An inverse design method for rail grinding profiles
A design method for rail profiles based on the geometric characteristics of wheel–rail contact
Inverse design of shock wave distortion for a direct-connect facility
Integration of Low-Fidelity MDO and CFD-Based Redesign of Low-Boom Supersonic Transports
Design studies on NAGIC flowfield with application to integrated irregular-shaped supersonic inlet
Integration of Low-Fidelity MDO and CFD-Based Redesign of Low-Boom Supersonic Transports
Integration of Low-Fidelity MDO and CFD-Based Redesign of Low-Boom Supersonic Transports
Inverse Design of Air-to-Air Missile System Based on Improved Genetic Algorithm
Research on Design Methods and Aerodynamics Performance of CQU-DTU-B21 Airfoil
Natural Laminar Flow Design for Highly Swept Wings
Parameter Space Exploration of Cellular Mechanical Metamaterials Using Genetic Algorithms
Inverse Design Method of Transonic Airfoil Based on Deep Neural Network
Assessment of Off-Design Low-Boom Characteristics of a Low-Boom Supersonic Transport
Assessment of Off-Design Low-Boom Characteristics of a Low-Boom Supersonic Transport
Assessment of Off-Design Low-Boom Characteristics of a Low-Boom Supersonic Transport
Gas dynamics analysis of an air pocket in the metal-stamping process
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport
Assessment of Off-Design Low-Boom Characteristics of a Low-Boom Supersonic Transport
Design of Optimum Torsionally Flexible PropRotors for Tilt-Body MAVs
Propulsion-Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport
Propulsion-Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport
Equivalent Area Targets for Inverse Design Optimization With Changing Low-Boom Cruise Conditions
Propulsion-Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport
Equivalent Area Targets for Inverse Design Optimization with Changing Low-Boom Cruise Conditions