Quantification of the boundary layer ingestion benet for the D8-series aircraft using a pressure rake system

Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2015.

Bibliographic Details
Main Author: Lieu, Michael K
Other Authors: Edward M. Greitzer, Mark Drela and Alejandra Uranga.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2015
Subjects:
Online Access:http://hdl.handle.net/1721.1/97264
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author Lieu, Michael K
author2 Edward M. Greitzer, Mark Drela and Alejandra Uranga.
author_facet Edward M. Greitzer, Mark Drela and Alejandra Uranga.
Lieu, Michael K
author_sort Lieu, Michael K
collection MIT
description Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2015.
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spelling mit-1721.1/972642019-04-10T21:34:00Z Quantification of the boundary layer ingestion benet for the D8-series aircraft using a pressure rake system Lieu, Michael K Edward M. Greitzer, Mark Drela and Alejandra Uranga. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2015. This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections. Cataloged from student-submitted PDF version of thesis. Includes bibliographical references (pages 141-142). This thesis presents the results of experiments carried out at NASA Langley Research Center (LaRC) 14'x22' Subsonic Wind Tunnel to determine the aerodynamic boundary layer ingestion (BLI) benet for the D8 aircraft advanced transport concept. The experiments involved a back-to-back comparison between two D8 aircraft configurations: a podded propulsion system (non-BLI) and a fuselage integrated propulsion system (BLI). The BLI benet was evaluated from ow surveys upstream and downstream of the propulsor using a rotating rake system for the two configurations. The BLI benefit, defined as the mechanical flow power saving at cruise conditions (zero net streamwise force), from the BLI configuration relative to the non-BLI configuration, was found to be 8.2% +/- 0:8%. The experimental-computational approach and the sensitivity analysis of the estimated BLI benefit to uncertainties such as flow angles and instrumentation errors are described in the thesis. The benefits and drawbacks of the rotating rake measurement technique used in the D8-series powered model aircraft experiments are also discussed. by Michael K. Lieu. S.M. 2015-06-10T18:41:03Z 2015-06-10T18:41:03Z 2015 2015 Thesis http://hdl.handle.net/1721.1/97264 910663150 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 142 pages application/pdf Massachusetts Institute of Technology
spellingShingle Aeronautics and Astronautics.
Lieu, Michael K
Quantification of the boundary layer ingestion benet for the D8-series aircraft using a pressure rake system
title Quantification of the boundary layer ingestion benet for the D8-series aircraft using a pressure rake system
title_full Quantification of the boundary layer ingestion benet for the D8-series aircraft using a pressure rake system
title_fullStr Quantification of the boundary layer ingestion benet for the D8-series aircraft using a pressure rake system
title_full_unstemmed Quantification of the boundary layer ingestion benet for the D8-series aircraft using a pressure rake system
title_short Quantification of the boundary layer ingestion benet for the D8-series aircraft using a pressure rake system
title_sort quantification of the boundary layer ingestion benet for the d8 series aircraft using a pressure rake system
topic Aeronautics and Astronautics.
url http://hdl.handle.net/1721.1/97264
work_keys_str_mv AT lieumichaelk quantificationoftheboundarylayeringestionbenetforthed8seriesaircraftusingapressurerakesystem