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ОбложкаHaxter S. Experimental evaluation of prediction models for coherence length and phase velocity of pressure fluctuations at flight conditions: Diss. … Dr.-Ing. / Deutsches Zentrum für Luft- und Raumfahrt, Institut für Aerodynamik und Strömungstechnik, Göttingen. - Köln: DLR, 2017. - viii, 112 p.: ill., tab. - (Forschungsbericht; 2017-57). - Res. also Germ. - Bibliogr.: p.97-104. - ISSN 1434-8454
Шифр:(Pr 1120/2017-57) 02

 

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Оглавление / Contents
 
1  Introduction ................................................. 1
   1.1  Objective und Outline of this Work ...................... 1
   1.2  State of the Art - Flight Test Array Measurements ....... 3
   1.3  State of the Art - Boundary Layer Phase Velocity
        Characteristics from Noisy Wind Tunnel Measurements ..... 6
   1.4  Restrictions on Using Flight Test Data .................. 9
2  Coherence of Surface Pressure: Flight Test Evaluation ....... 11
   2.1  Models for Comparison: Coherence Length ................ 11
   2.2  Experimental Setup ..................................... 18
   2.3  Data Processing ........................................ 28
   2.4  Data Quality ........................................... 34
   2.5  Results ................................................ 42
3  Phase Velocity of Surface Pressure: Wind Tunnel Test
   Evaluation .................................................. 51
   3.1  Experimental Setup ..................................... 51
   3.2  Data Processing and Methods ............................ 55
   3.3  Existing phase velocity prediction models .............. 58
   3.4  Results ................................................ 60
4  Discussion .................................................. 75
   4.1  Coherence Evaluation ................................... 75
   4.2  Phase Evaluation ....................................... 78
5  Summary ..................................................... 85
   5.1  Coherence Evaluation ................................... 85
   5.2  Phase Evaluation ....................................... 86
   5.3  Conclusion ............................................. 88
6  Outlook ..................................................... 89
Nomenclature ................................................... 91
Bibliography ................................................... 97
A  Appendix ................................................... 105
   A.l  Deriving the flow angle from the coherence over the
        array ................................................. 105
   A.2  Generation of Numerical Data .......................... 110


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