4.3 Article

Design optimization of a wind tunnel force balance using stepwise response surface method

Journal

JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY
Volume 36, Issue 6, Pages 3071-3079

Publisher

KOREAN SOC MECHANICAL ENGINEERS
DOI: 10.1007/s12206-022-0537-4

Keywords

Force balance; Response surface methodology; Optimization; Regression

Funding

  1. NASA Langley Research Center [17947, 18994]
  2. University of Maryland at Baltimore County, Department of Mechanical Engineering [3000633775]

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This paper proposes a stepwise response surface method for the design optimization of a force balance. Through broad and narrow sampling trials, a quadratic model was generated to determine the final optimum point. The final design of the force balance ensures satisfactory gauge readings and decreased stress values.
A force balance measures the forces being applied to an object in a wind tunnel test. The force balance needs to be optimized to generate an acceptable gauge reading while guaranteeing no structural failure by the wind tunnel loadings. This paper proposes a stepwise response surface method (RSM) for design optimization of a force balance. Three sampling techniques were tried in the RSM study, and finite element simulation was used for functional evaluation. The first trial was based on broad sampling, followed by a second trial based on narrow sampling. The data from these trials was then utilized in a final regression, in which a quadratic model was generated to identify the final optimum point. The final design of the force balance provides satisfactory gauge readings with decreased stress values even though the roll moment is greatly increased.

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