A Python implementation of the 1976 standard atmosphere model. Suitable to determine air properties at different altitudes.
Flight Dynamics Project - UAV
Program translates MSC Nastran Cquad elements with 1D Crod on leading edge to CAERO1 elements with generation of d2wgj, wkk and f2gj matricles.
Aynı Ailden 2 Şok Dalgasının Kesişmesi Sonucu Oluşacak Akışın Genel Özelliklerini Hesaplamaktadır.
Using Neural Networks to predict Aerodynamic coefficients of out of distribution Aerofoils
It calculates the general properties of the flow that will occur as a result of the intersection of two shock waves from the same family.
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