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Flexible Twist for Pitch Control in a High Altitude Long Endurance Aircraft With Nonlinear Response
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Flexible Twist for Pitch Control in a High Alti... 1025088794 Book Cover

Flexible Twist for Pitch Control in a High Alti...

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Edition Description

The goal was to demonstrate that scaling the nonlinear response of a full-scale finite element model of a high-altitude long-endurance (HALE) aircraft was possible if the model was aeroelastically and "nonlinearly" scaled. A straight-forward method of scaling the first three...

Edition Details
Format:Hardcover
Language:English
ISBN:1025088794
Format: Hardcover
Condition:
$
32.95
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