Wing Structure of Advanced Supersonic Trainer

The Lift of a Delta Wing at Supersonic Speeds*

Multiobjective evolutionary computation for supersonic wing-shape optimization

This paper discusses the design optimization of a wing for supersonic transport (SST) using a multiple-objective genetic algorithm (MOGA). Three objective functions are used to minimize the drag for supersonic cruise, the drag for transonic cruise, and the bending moment at the wing root for supersonic cruise. The wing shape is defined by 66 design variables. A Euler flow code is used to evalua...

Oscillating Supersonic delta wing with Straight Leading Edges

A Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with straight leading edge for the attached shock case. Ghosh’s strip theory is been used in which strips at different span wise locations are independent of each other. This combines with the similitude to give a piston theory which gives the closed form of solution to stability derivatives ...

Desdemona: Advanced Disorientation Trainer and (sustained-G) Flight Simulator

Desdemona is a sophisticated demonstration, simulation, training and research facility specified by TNO Human Factors and developed by AMST Systemtechnik. The Desdemona concept adds a sustainable G-load to the conventional Stewart platform motion, without the angular accelerations encountered in centrifuges during the G-onset. This is accomplished by having the aviator sitting in a fully gimbal...

prediction of aerodynamic coefficients of a supersonic wing using boundary element method

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