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

Download this report (PDF, 2.74 MB, 140 pages)

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

Abstract:
The abstract for this report is either unavailable or has yet to be entered

Provenance: Lockheed Martin Missiles & Fire Control

Contact us about this report

Other options for obtaining this report:

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a pdf download of the report, exists at DTIC

Via National Technical Report Library:
This report may be available for download from NTRL. Use the Title from this record to locate the item in DTIC Online

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement