Volume IV. Wind Tunnel Test of the Concersion Process of a Folding Tilt-Rotor Aircraft Using a Semispan Unpowered Model: Part II. Blade Stress Analysis, Bench Tests, and Wind Tunnel Model Details
Report Number: AFFDL TR 71-62 Volume 4 Part 2
Author(s): Magee, John, Taylor, Robert
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-08
Pages: 83
Contract: F33615-69-C-1577
DoD Project: 69BT
Identifier: AD0735733
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Magee, John, Taylor, Robert
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-08
Pages: 83
Contract: F33615-69-C-1577
DoD Project: 69BT
Identifier: AD0735733
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control