| Summary of Design Activities in LARA Task 1.2 (1995) | |||||||||
Abstract | |||||||||
| This report describes a comparison of wing design results of a selected test case of a laminar flow wing obtained in the EU-Programme APAS/LARA, Task 1.2 by various partners involved with different methods. The results show that good progress has been obtained in wing design methods and that a laminar flow wing design with a prescribed pressure distribution for a given planform can be performed with high confidence. | |||||||||
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