Inlet drag prediction for aircraft conceptual design

A research effort aimed at enhancing ACSYNT, a computer program for aircraft conceptual design, has necessitated the development of methods for predicting inlet drag. Originally, the drag of only one inlet type, the variable-geometry conical inlet, could be calculated within ACSYNT. This prompted th...

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Bibliographic Details
Main Author: Malan, Paul
Other Authors: Mechanical Engineering
Format: Others
Published: Virginia Polytechnic Institute and State University 2015
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