Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part II. Experimental And Theoretical Data For Bare wings And wings with Tip Tanks

Item

Title
Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part II. Experimental And Theoretical Data For Bare wings And wings with Tip Tanks
Date
1955
Index Abstract
Coming Soon
Photo Quality
Complete
Report Number
WADC TR 54-113 Part 2
Creator
McCarthy, John F., Jr.
Martuccelli, John R.
Asher, Gifford W.
Zartarian, Garabed
Corporate Author
Massachusetts Institute of Technology
Laboratory
Aircraft Laboratory
Extent
245
NTRL Accession Number
AD110593
Identifier
AD0110593
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
None
Report Availability
Full text available
Date Issued
1955-12
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