Transition Prediction and Analysis of the CRM-NLF Wing with the DLR TAU Code
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-030-79561-0_18
Reference17 articles.
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3. Lynde, M.N., et al.: Preliminary results from an experimental assessment of a natural laminar flow design method. In: AIAA SCITECH Forum (2019)
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5. Seitz, A., Hübner, A., Risse, K.: The DLR TuLam project: design of a short and medium range transport aircraft with forward swept NLF wing. CEAS Aeronaut. J. 11(2), 449–459 (2019). https://doi.org/10.1007/s13272-019-00421-1
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