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

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

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Provenance: Lockheed Martin Missiles & Fire Control

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