Nonlinear Thermoelasitc Effects on Hypersonic Stability and Control, Part III: Simulation, Measurement and Analysis of Nonlinear Static Aerothermoelastic Behavior of a 45 Degree Delta Wing

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Report Number: FDL TDR 64-16 Part 3
Author(s): Batt, James R.
Corporate Author(s): Bell Aerosystems Co.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-02
Pages: 58
Contract: AF 33(657)-7486
DoD Project: 8219
DoD Task: 821901
Identifier: AD0613708

Results are presented of additional nonlinear structuralaerodynamic interaction experiments and analyses conducted on a 45 degree delta wing. The aeroelastic simulation scheme developed and described in AD-608 476 was used to experimentally determine the static aerothermoelastic behavior of the subject model wing. Test data were compared with theoretical predictions using a digital computer program.

Provenance: Lockheed Martin Missiles & Fire Control

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