columbus · 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

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

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