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Schülein, Erich (2016) Simplified model for flow-heating effect on wave drag and its validation. AIAA Journal, 54 (3), pp. 1030-1039. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J054604. ISSN 0001-1452.
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Official URL: http://arc.aiaa.org/doi/abs/10.2514/1.J054604
Abstract
A simplified prediction method for determination of flow-heating effects on the wave drag of bodies based on the combined analytical–empirical model of the thermal-spike phenomenon is presented. The existing model conceptions addressing certain aspects of this phenomenon were complemented and refined to develop a method suitable for parameter studies. Some reliable experimental and numerical results for the Mach 3 supersonic flow over conically nosed bodies were used as training data to estimate empirically the model parameters. Finally, the method was cross validated by the different available results for blunt bodies with hemispherical, flat, and conical front faces. By this opportunity, the ability to predict the influence of some crucial parameters has successfully been demonstrated for the heat input ratio at steady and periodic heating, the normalized heated-wake/filament diameter, the Mach number, and the specific heat capacity. Read More: http://arc.aiaa.org/doi/abs/10.2514/1.J054604
| Item URL in elib: | https://elib.dlr.de/102874/ | ||||||||
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| Document Type: | Article | ||||||||
| Additional Information: | March 2016, Publication Date (online): December 21, 2015 | ||||||||
| Title: | Simplified model for flow-heating effect on wave drag and its validation | ||||||||
| Authors: |
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| Date: | 2016 | ||||||||
| Journal or Publication Title: | AIAA Journal | ||||||||
| Refereed publication: | Yes | ||||||||
| Open Access: | Yes | ||||||||
| Gold Open Access: | No | ||||||||
| In SCOPUS: | Yes | ||||||||
| In ISI Web of Science: | Yes | ||||||||
| Volume: | 54 | ||||||||
| DOI: | 10.2514/1.J054604 | ||||||||
| Page Range: | pp. 1030-1039 | ||||||||
| Publisher: | American Institute of Aeronautics and Astronautics (AIAA) | ||||||||
| ISSN: | 0001-1452 | ||||||||
| Status: | Published | ||||||||
| Keywords: | supersonic flow, energy deposition, wave-drag reduction, conical nose, hemispherical nose | ||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||
| HGF - Program: | Aeronautics | ||||||||
| HGF - Program Themes: | fixed-wing aircraft | ||||||||
| DLR - Research area: | Aeronautics | ||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||
| DLR - Research theme (Project): | L - Military Technologies (old) | ||||||||
| Location: | Göttingen | ||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > High Speed Configurations | ||||||||
| Deposited By: | Bachmann, Barbara | ||||||||
| Deposited On: | 12 May 2016 16:57 | ||||||||
| Last Modified: | 31 Oct 2023 11:09 |
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