Compressible Boundary-Layer Stability Calculations for Sweptback Wings with Suction (Q3947367): Difference between revisions
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Latest revision as of 14:39, 19 March 2024
scientific article
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Compressible Boundary-Layer Stability Calculations for Sweptback Wings with Suction |
scientific article |
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Compressible Boundary-Layer Stability Calculations for Sweptback Wings with Suction (English)
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1982
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wings of infinite span
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compressible, parallel-flow stability theory
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supercritical
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sweep angle of 23 deg, 35 deg
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maximum spatial amplification rate
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suction
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maximum amplification rate
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