Haxter, Stefan and Spehr, Carsten (2013) Examination of the Influence of Flight Altitude and Speed on the Efimtsov Model Parameters. In: 19th AIAA/CEAS Aeroacoustics Conference (AIAA 2), pp. 1-27. American Institute of Aeronautics and Astronautics Inc.. 19th AIAA/CEAS Aeroacoustics Conference (34th AIAA Aeroacoustics Conference), 2013-05-27 - 2013-05-29, Berlin, Germany. doi: 10.2514/6.2013-2028. ISBN 978-162410213-4.
|
PDF
2MB |
Official URL: https://doi.org/10.2514/6.2013-2028
Abstract
A flight test was conducted and the data was evaluated in order to investigate the influence of flight altitude and flight speed on the coherence length model by Efimtsov. An underestimation of the measured values by the model was found below a frequency of 1kHz. Above this frequency, the predicted values matched the measured values very well. The Efimtsov ansatz was found to be suitable for the description of coherence length, when the parameters are adapted. Three further analyses were performed: the flight speed was varied with constant altitude, the altitude was varied with constant flight speed, and both speed & altitude were varied together. No considerable variation was measured when the flight speed was varied separately. A small variation was determined at low frequency when the flight altitude was altered separately. When varying the parameters together, a distinct variation was found for the cases of highest speed and altitude. The applicability of the exponential coherence decay was analyzed. The absolute deviation was found to increase with lower frequency. The characteristic of the deviation was found to collapse in different regions with different scaling of the strouhal number.
| Item URL in elib: | https://elib.dlr.de/77817/ | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||
| Additional Information: | DOI: 10.2514/6.2013-2028 | ||||||||||||
| Title: | Examination of the Influence of Flight Altitude and Speed on the Efimtsov Model Parameters | ||||||||||||
| Authors: |
| ||||||||||||
| Date: | 24 May 2013 | ||||||||||||
| Journal or Publication Title: | 19th AIAA/CEAS Aeroacoustics Conference | ||||||||||||
| Refereed publication: | No | ||||||||||||
| Open Access: | Yes | ||||||||||||
| Gold Open Access: | No | ||||||||||||
| In SCOPUS: | Yes | ||||||||||||
| In ISI Web of Science: | No | ||||||||||||
| DOI: | 10.2514/6.2013-2028 | ||||||||||||
| Page Range: | pp. 1-27 | ||||||||||||
| Editors: |
| ||||||||||||
| Publisher: | American Institute of Aeronautics and Astronautics Inc. | ||||||||||||
| Series Name: | Conference Proceedings online | ||||||||||||
| ISBN: | 978-162410213-4 | ||||||||||||
| Status: | Published | ||||||||||||
| Keywords: | turbulent boundary layer, coherence length model, | ||||||||||||
| Event Title: | 19th AIAA/CEAS Aeroacoustics Conference (34th AIAA Aeroacoustics Conference) | ||||||||||||
| Event Location: | Berlin, Germany | ||||||||||||
| Event Type: | international Conference | ||||||||||||
| Event Start Date: | 27 May 2013 | ||||||||||||
| Event End Date: | 29 May 2013 | ||||||||||||
| Organizer: | American Institute of Aeronautics and Astronautics | ||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||
| HGF - Program Themes: | Aircraft Research (old) | ||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||
| DLR - Research theme (Project): | L - Simulation & Validation (old) | ||||||||||||
| Location: | Göttingen | ||||||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > Experimental Methods, GO | ||||||||||||
| Deposited By: | Micknaus, Ilka | ||||||||||||
| Deposited On: | 22 Aug 2013 13:32 | ||||||||||||
| Last Modified: | 24 Apr 2024 19:44 |
Repository Staff Only: item control page