columbus · 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

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

Title: 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
Date: 1971
Index Abstract: Not Available
Photo Quality: Complete
Report Number: AFFDL TR 71-62 Volume 4 Part 2
Creator: Magee, John; Taylor, Robert
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 83
Identifier: AD0735733
Access Rights: Approved for Public Release Distribution Unlimited
Distribution Classification: 1
Contract: F33615-69-C-1577
DoD Project: 69BT
DoD Task: None Given
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Full text available
Date Issued: 1971-08
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control; AFRL/VACA
Type: report
Format: 1 online resource