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- Subject Heading...is e(N) method natural laminar flow wing flight test wind tunnel test
Inverse wing design for the scaled supersonic experimental airplane with ensuring design constraints
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- Subject Heading...ign constraint natural laminar flow wing wing section geometry thickne...
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- Subject Heading...yer transition natural laminar flow wing e(exp N) method compressible ...
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- Subject Heading...namical design natural laminar flow wing computational fluid dynamics ...
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- Subject Heading...ental airplane natural laminar flow wing turbulent boundary layer tran...
- Note (General)...urement on the natural laminar flow wing of non-powered experimental a...
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- Subject Heading...ow flight test natural laminar flow wing CFD technique computational f...
- Note (General)...igned to apply natural laminar flow wing using CFD (Com...... to X/C = 0.5. Natural laminar flow wing is expected to realize on the...
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