Titlebook: Design and Development of Aerospace Vehicles and Propulsion Systems; Proceedings of SAROD S. Kishore Kumar,Indira Narayanaswamy,V. Ramesh C

Eeg332

Multi-fidelity Aerodynamic Optimization of an Airfoil at a Transitional Low Reynolds Number,sitional low Reynolds number (Re?=?5?×?10.) using surrogate-based optimization technique. Bezier curves are used to parameterize the airfoil. Latin hypercube sampling (LHS) technique is used to sample the initial set of samples. The aerodynamic response is estimated using low- and high-fidelity data

獸群

Aerodynamic Optimization of Transonic Wing for Light Jet Aircraft, Light jets often cruise at high subsonic Mach numbers enabling greater range. Consequently, the drawback associated with high Mach number flight is that it leads to the deterioration of the aircraft’s aerodynamic characteristics. Aerodynamic optimization of a typical transonic wing was performed to

舊石器

Intercept