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

Item

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