Inertia Measurement and Dynamic Stability Analysis of a Radio-Controlled Joined-Wing Aircraft

Language: English

Published by Creative Media Partners, LLC Okt 2012, 2012

1249596297 / 9781249596295

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Seller: AHA-BUCH GmbH, Einbeck, GermanyAHA-BUCH GmbH

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Neuware - Dynamic stability and stall during steady level turns were examined for VA-1, a joined-wing flight demonstrator aircraft. Configurations with a lower vertical tail and fairings over the main landing gear were compared with a recommendation on the combination had the best drag and dynamic stability characteristics. The dynamic stability analysis was broken into four key parts: a twist test experimentally measured mass moments of inertia, a panel method was used to find non-dimensional stability derivatives, lateral and longitudinal state space models estimated dynamic stability characteristics and handling quality levels were evaluated using a Cooper-Harper based rating system. VA-1 was found to have good longitudinal and lateral flight qualities for cruise flight. The lower vertical tail could be removed to reduce weight and drag without degrading dynamic stability. Spanwise lift coefficients for different wing sections in trimmed steady state turns at 50 and 55 degrees of bank were estimated to see which sections of the wing stalled first. The analysis revealed VA-1 can turn using bank angles less than 50 degrees without stall and that stall first occurred at the aileron, immediately outboard of the wing joint.

Seller Inventory # 9781249596295

Title
Inertia Measurement and Dynamic Stability Analysis of a Radio-Controlled Joined-Wing Aircraft
Author
William A McClelland
Publisher
Creative Media Partners, LLC Okt 2012
Publication year
2012
Condition
Neu
Binding
Taschenbuch
Language
English
ISBN 10
1249596297
ISBN 13
9781249596295
Item weight
159 grams
Dimensions
234x156x6 mm

AHA-BUCH GmbH

Einbeck, Germany

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