A Review of Boundary Layer Ingestion Modeling Approaches for Use in Conceptual Design

Hendricks, Eric S

关键词: AIRCRAFT PERFORMANCE;    BOUNDARY LAYER INGESTION PROPULSION;    AERODYNAMIC STALLING;   

RP-ID  :  NASA/TM-2018-219926,E19542,GRC-E-DAA-TN57522

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

The concept of boundary layer ingestion (BLI) has been proposed by NASA researchers and other groups for improving the performance of a number of future aircraft concepts. These future aircraft concepts include the STARC-ABL, D8 and N-3X among other examples. While BLI technology appears to be promising for improving the aircraft performance by reducing fuel burn, the benefits and challenges of using this technology are not well understood. As a result, there are a number of e orts ongoing within NASA which are attempting to model BLI and determine its overall bene t. Despite their common goal, there seems to be significant differences in the modeling approaches used in each e ort, with limited communication and collaboration between these groups. The purpose of this report is to document NASA's in-house BLI modeling e orts and their associated methodologies. Furthermore, the report will identify strengths and weaknesses of each methodology, specifically in regards to each method's application in conceptual design.