Experimental Investigation of the Flow Mechanisms Associated with a Wake-Ingesting Propulsor-Reference-Cited by-同舟云学术

Experimental Investigation of the Flow Mechanisms Associated with a Wake-Ingesting Propulsor

Published:2017-04 Issue:4 Volume:55 Page:1332-1342
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Lv P.¹,Ragni D.¹,Hartuc T.¹,Veldhuis L.¹,Rao A. G.¹

Affiliation:

1. Delft University of Technology, 2629 HS Delft, The Netherlands

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055292

Reference37 articles.

1. GreitzerE.BonnefoyP.De la Rosa BlancoE.DorbianC.DrelaM.HallD.HansmanR.HilemanJ.LiebeckR.LovergrenJ. “N+3 Aircraft Concept Designs and Trade Studies Final Report,” NASA John H. Glenn Research Center CR-2010-216794/vol2, Cleveland, OH, Jan. 2010.

2. KawaiR. T.FriedmanD. M.SerranoL. “Blended Wing Body (BWB) Boundary Layer Ingestion (BLI) Inlet Configuration and System Studies,” NASA Rept. CR-214534, Dec. 2006.

3. Development of the D8 Transport Configuration

4. Airframe Design for Silent Fuel-Efficient Aircraft

5. Control Volume Analysis of Boundary Layer Ingesting Propulsion Systems With or Without Shock Wave Ahead of the Inlet

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