PAN AIR applications to aero-propulsion integration
| العنوان: | PAN AIR applications to aero-propulsion integration |
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| المؤلفون: | Edward N. Tinoco, Allen W Chen |
| المصدر: | Journal of Aircraft. 21:161-167 |
| بيانات النشر: | American Institute of Aeronautics and Astronautics (AIAA), 1984. |
| سنة النشر: | 1984 |
| مصطلحات موضوعية: | Nacelle, Internal flow, business.industry, Mass flow, Nozzle, Aerospace Engineering, Propulsion, Compressible flow, Power (physics), External flow, Boundary layer, Calibration, Environmental science, Aerospace engineering, business, Propulsive efficiency |
| الوصف: | The versatility of the PAN AIR system has led to its application to a variety of aero-propulsion problems. Examples of some of these applications on subsonic transport configurations are presented to illustrate the use of the PAN AIR system. The cases presented include one example in which PAN AIR was coupled to threedimensional boundary layer analysis for iterative solutions. An internal flow case and several external flow cases are presented. These include a study of the internal flow losses through a calibration nozzle, the calculation of surface pressures about an isolated nacelle, the modeling of exhaust flows, and the analysis of nacelle blowing (power) effects on a complete wing-body-strut-nacelle configuration. |
| تدمد: | 1533-3868 0021-8669 |
| URL الوصول: | https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c652410a0294c39fba2bb3a760fbda86 https://doi.org/10.2514/3.48241 |
| رقم الأكسشن: | edsair.doi.dedup.....c652410a0294c39fba2bb3a760fbda86 |
| قاعدة البيانات: | OpenAIRE |
| تدمد: | 15333868 00218669 |
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