کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
1717625 | 1520084 | 2016 | 8 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
An assessment of distributed propulsion: Part B – Advanced propulsion system architectures for blended wing body aircraft configurations
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موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی هوافضا
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: An assessment of distributed propulsion: Part B – Advanced propulsion system architectures for blended wing body aircraft configurations An assessment of distributed propulsion: Part B – Advanced propulsion system architectures for blended wing body aircraft configurations](/preview/png/1717625.png)
چکیده انگلیسی
Studies such as those by NASA predict large performance benefits when integrating Distributed Propulsion (DP) with the Blended Wing Body (BWB) aircraft configuration. This is because the BWB planform geometry is particularly suited to the ingestion of boundary layer air. The present study evaluates the relative benefit of DP through a comparison with an advanced turbofan reference system of the same technology level as in Part A of this two part paper. Fuel savings of 5.3% relative to the reference aircraft have been shown to be achievable, although it was found that the system is particularly sensitive to duct losses.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 50, March 2016, Pages 212–219
Journal: Aerospace Science and Technology - Volume 50, March 2016, Pages 212–219
نویسندگان
Rudi Kirner, Lorenzo Raffaelli, Andrew Rolt, Panagiotis Laskaridis, Georgios Doulgeris, Riti Singh,