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History/Military Gust Load Prediction and Alleviation on a Fighter Aircraft: Jargen Becker

Posted on 2010-03-16




Name:History/Military Gust Load Prediction and Alleviation on a Fighter Aircraft: Jargen Becker
ASIN/ISBN:9283515323
Language:English
File size:1.94 Mb
ISBN: 9283515323
Publish Date: 1985
File Type: PDF (OCR)
Pages: 28 pages
File Size: 1.94 Mb
Other Info: Advisory Group for Aerospace Research and Development (AGARD)
   History/Military Gust Load Prediction and Alleviation on a Fighter Aircraft: Jargen Becker

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Gust Load Prediction and Alleviation on a Fighter Aircraft: Jargen Becker

Description: Turbulence induced dynamic loads and vibrations on a fighter aircraft may play a considerable role for certain configurations with respect to the design of the structure and the performance of special missions or they may cause on the other hand limitations of the flight envelope.

As far as aircombat aircraft are concerned typical restrictions may be found for instance with respect to design gust loads if wing tip mounted store configurations are investigated or with respect to ride comfort if low level high speed missions are evaluated.

Here both aspects namely design gust critical cases and ride comfort are therefore reported in more detail in order to demonstrate the problem areas. In this context also some difficulties of turbulence response prediction methods will be described, especially with respect to the dynamics of the aircraft with FCS and the interaction of flight and structural dynamics, though these methods are well established. In addition problem areas of the aircraft with FCS and gust alleviation system are mentioned for the case of ride improvement. The design of such systems would strongly necessitate the full dynamic description of the flexible fighter aircraft in order to evaluate maximum loads, fatigue loads and structural coupling problems with the control system.

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