Evaluation of Three-Dimensional Transonic Methods for the Analysis of Figrter Configurations

Bhateley, Ishwur; Mann, Michael J.; Ballhaus, W. F.

doi:10.2514/6.1979-1528

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Test-to-theory Comparisons1

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1981

1983

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Cited by 6 publications

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“…This choice was based on test-to-theory correlations made in an earlier study. 19 Results there showed that the highly swept strake produced a mathematically unacceptable skewed mesh arrangement.…”

Section: Test-to-theory Comparisonsmentioning

confidence: 99%

Design, analyses, and model tests of an aeroelastically tailored lifting surface

Rogers

Braymen

Shirk

1983

Journal of Aircraft

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Aeroelastic tailoring provides a measure of control over the interaction of aerodynamic loading and structural response during the design of composite lifting surfaces. A recent investigation involving the design, fabrication, and test of an aeroelastically tailored fighter wing was conducted to provide data for validating the design methodology. Three sets of composite wings with different design objectives were tested in addition to a set of rigid steel wings. The static aeroelastic tests featured the measurement of model forces, pressure distributions, and deflected shapes in the transonic regime. Test results are compared with analytical predictions and show significant aeroelastic benefits.

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Section: Test-to-theory Comparisonsmentioning

confidence: 99%