OPTIMAL DESIGN OF ROTOR BLADE FOR A WINGED COMPOUND HELICOPTER AT HIGH ADVANCE RATIO

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OPTIMAL DESIGN OF ROTOR BLADE FOR A WINGED COMPOUND HELICOPTER AT HIGH ADVANCE RATIO

OPTIMAL DESIGN OF ROTOR BLADE FOR A WINGED COMPOUND HELICOPTER AT HIGH ADVANCE RATIO

Sugiura, M. / Tanabe, Y. / Sugawara, H.

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Title :

OPTIMAL DESIGN OF ROTOR BLADE FOR A WINGED COMPOUND HELICOPTER AT HIGH ADVANCE RATIO

Contributors:

Sugiura, M. (author) / Tanabe, Y. (author) / Sugawara, H. (author)

Conference:

76th Annual Vertical Flight Society Forum and Technology Display (Forum 76) : the future of vertical flight. Vol 3 (Online)

Published in:

76th Annual Vertical Flight Society Forum and Technology Display (Forum 76) : the future of vertical flight. Vol 3 (Online) ; 1895-1902

Annual forum proceedings ; 76

Publication date :

2020-01-01

Size :

8 pages

ISSN :

Type of media :

Conference paper

Type of material :

Print

Language :

English

© Metadata Copyright the British Library Board and other contributors. All rights reserved.

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