Bohnke D. A multi-fidelity workflow to derive physics-based conceptual design methods: Diss. … Dr.-Ing. / Deutsches Zentrum für Luft- und Raumfahrt, Lufttransportsysteme, Hamburg. - Köln: DLR, 2015. - XV, 189 p.: ill. - (Forschungsbericht; 2015-09). - Res. also Germ. - Bibliogr.: p. 145-157. - ISSN 1434-8454  Место хранения:   02 | Отделение ГПНТБ СО РАН | Новосибирск

Оглавление / Contents

1 Introduction ................................................. l 1.1 Situation ............................................... l 1.2 Problem Definition ...................................... 6 1.3 Solution ................................................ 8 1.4 Outline ................................................ 15 2 State of the Art ............................................ 17 2.1 Conceptual Design ...................................... 19 2.2 Design Environments .................................... 25 2.3 Multi-Fidelity ......................................... 33 2.4 Surrogate Models ....................................... 39 3 Multi-Fidelity Workflow ..................................... 51 3.1 Conceptual Design ...................................... 55 3.2 Multi-Fidelity ......................................... 63 3.3 Design of Experiments .................................. 68 3.4 Symbolic Regression .................................... 75 4 Design Studies .............................................. 89 4.1 Oswald Factor .......................................... 89 4.2 Wing Mass ............................................. 107 4.3 Strut-Braced Wing Mass ................................ 121 5 Discussion ................................................. 131 6 Conclusion ................................................. 137 Bibliography .................................................. 144 A Complexity ................................................. 159 В Validation Data ............................................ 161 С Design of Experiments ...................................... 167 D Oswald Factor .............................................. 171 E Wing Mass .................................................. 175 F Strut Braced Wing Mass ..................................... 179