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Investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30(degree) sweptback wing at transonic speeds

By: Charles F Whitcomb.

Contributor(s): Philippa F Brown.

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BookPublisher: DDC classification: NASA | TN D-620 -

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-620 - (Browse shelf)	Not for loan		TR10235

Total holds: 0

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