Acta mechanica Sinica, 2011-04, Vol.27 (2), p.152-163
2011
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Details
- Autor(en) / Beteiligte
- Titel
- Aerodynamics of indirect thrust measurement by the impulse method
- Ist Teil von
- Acta mechanica Sinica, 2011-04, Vol.27 (2), p.152-163
- Ort / Verlag
- Heidelberg: The Chinese Society of Theoretical and Applied Mechanics, Institute of Mechanics, Chinese Academy of Sciences
- Erscheinungsjahr
- 2011
- Quelle
- SpringerLink
- Beschreibungen/Notizen
- The aerodynamic aspects of indirect thrust measurement by the impulse method have been studied both experimentally and numerically. The underlying basic aerodynamic principle is outlined, the phenomena in subsonic, supersonic and arc-heated jets are explored, and factors affecting the accuracy of the method are studied and discussed. Results show that the impulse method is reliable for indirect thrust measurement if certain basic requirements are met, and a simple guideline for its proper application is given.
- Sprache
- Englisch
- Identifikatoren
- ISSN: 0567-7718eISSN: 1614-3116DOI: 10.1007/s10409-011-0431-2Titel-ID: cdi_proquest_miscellaneous_914626534
- Format
- –
- Schlagworte
- Aerodynamics, Classical and Continuum Physics, Computational Intelligence, Engineering, Engineering Fluid Dynamics, Guidelines, Impulses, Jets, Mathematical models, Research Paper, Subsonic aircraft, Supersonic aircraft, Theoretical and Applied Mechanics, Thrust measurement, 亚音速, 影响因素, 推力测量, 测量方法, 电弧加热, 空气动力学原理, 脉冲法