Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 3: Experimental and Theoretical Data for Wings with Control Surfaces
Report Number: WADC TR 54-113 Part 3
Author(s): Asher, Gifford W., Weatherhill, Warren H.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-01
Pages: 95
Contract: AF 33(038)-22955
DoD Project: 1370
DoD Task: 13474
Identifier: AD0118052
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Asher, Gifford W., Weatherhill, Warren H.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-01
Pages: 95
Contract: AF 33(038)-22955
DoD Project: 1370
DoD Task: 13474
Identifier: AD0118052
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control