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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

Report Number: WADC TR 54-113 Part 2
Author(s): John F. McCarthy Jr.; Garabed Zartarian; John R. Martuccelli; Gifford W. Asher
Corporate Author: Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Pages: 245
Contract: AF 33(038)-22955
Project: 1370
Task: 13474
AD Number: AD0110593

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