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Select ADO-DG Case Studies in Aerodynamic Design Optimization。
Capability to predict the flow past an airplane in different flight regimes such as take off, cruise, flutter. 2 Interactive design calculations to allow immediate improvement 3 A...
A light structure is needed to reduce W0. SFC is the province of the engine manufacturers. The aerodynamic designer should try to maximize VL D . This means the cruising speed V should be increase...
For a given stress σ, the required skin thickness varies inversely as the wing depth d. Thus weight can be reduced by increasing the thickness to chord ratio. But this will increase shock drag in th...
The computation of boundary layer properties and laminar-to-turbulent transition location is a very complex problem, generally not undertaken in the context of aircraft design. Yet if an aircraft i...
Growing interest in micro-air-vehicles has created the need for improved understanding of the relevant aerodynamics. A reasonable starting point is the study of airfoil aerodynamics at Reynolds nu...
An aerodynamic design criterion was discussed for the 1+3/2 counter-rotating turbine by analyzing the velocity triangles. There are 8 key aerodynamic parameters in the criterion, based on the consider...

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