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An efficient method for predicting zero-lift or boundary-layer drag including aeroelastic effects for the design environment.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1221, p. 1451, doi. 10.1017/S0001924000011349
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- Publication type:
- Article
On a cellular division method for aircraft structural design.
- Published in:
- Aeronautical Journal, 2009, v. 113, n. 1150, p. 821
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- Publication type:
- Article