columbus · Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 3: Experimental and Theoretical Data for Wings with Control Surfaces

Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 3: Experimental and Theoretical Data for Wings with Control Surfaces

Title: Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 3: Experimental and Theoretical Data for Wings with Control Surfaces
Date: 1958
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: WADC TR 54-113 Part 3
Creator: Asher, Gifford W.; Weatherhill, Warren H.
Corporate Author: Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Extent: 95
NTRL Accession Number: AD118052
Identifier: AD0118052
Access Rights: ASTIA
Distribution Classification: 1
Contract: AF 33(038)-22955
DoD Project: 1370
DoD Task: 13474
DTIC Record Exists: No
Distribution Change Authority Correspondence: AFAL LTR
Report Availability: Full text available
Date Issued: 1958-01
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource