Volume IV. Wind Tunnel Test of the Conversion Process of a Folding Tilt-Rotor Aircraft Using a Semispan Unpowered Model: Part I. Analysis and Results

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Report Number: AFFDL TR 71-62 Volume 4 Part 1
Author(s): Magee, John, Taylor, Robert
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-08
Pages: 140
Contract: F33615-69-C-1577
DoD Project: 69BT
Identifier: AD0735632

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Provenance: Lockheed Martin Missiles & Fire Control

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