columbus · Wind Tunnel Tests of a Free-Wing Tilt-Propeller V/STOL Airplane Model

Wind Tunnel Tests of a Free-Wing Tilt-Propeller V/STOL Airplane Model

Title: Wind Tunnel Tests of a Free-Wing Tilt-Propeller V/STOL Airplane Model
Date: 1969
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: AFFDL TR 69-80
Creator: Strand, T.; Levinsky, E. S.
Corporate Author: Air Vehicle Corporation
Extent: 62
NTRL Accession Number: AD698355
Identifier: AD0698355
Access Rights: This document has been approved for public release and sale: its distribution is unlimited.
Distribution Classification: 1
Contract: F33615-68-C-1672
DoD Project: None Given
DoD Task: None Given
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Full text available
Date Issued: 1969-10
Abstract: The abstract for this report is either unavailable or has yet to be entered
Laboratory: Air Force Flight Dynamics Laboratory
Provenance: Lockheed Martin Missiles & Fire Control; AFRL/VACA
Type: report
Format: 1 online resource