Convoluted Intake Distortion Measurements Using Stereo Particle Image Velocimetry-Reference-Cited by-同舟云学术

Convoluted Intake Distortion Measurements Using Stereo Particle Image Velocimetry

Published:2017-06 Issue:6 Volume:55 Page:1878-1892
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Gil-Prieto Daniel¹,MacManus David G.¹,Zachos Pavlos K.¹,Tanguy Geoffrey¹,Menzies Kevin R.²

Affiliation:

1. Cranfield University, Cranfield, England MK43 0AL, United Kingdom

2. Rolls-Royce, Bristol, England BS34 7QE, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055467

Reference36 articles.

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

2. Flow Simulation of N2B Hybrid Wing Body Configuration

3. “A Methodology for Assessing Inlet Swirl Distortion,” Society of Automotive Engineers Rept. 5686, Warrendale, PA, 2007.

4. “Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines,” Society of Automotive Engineers Rept. 1419a, Warrendale, PA, 1999.

Cited by 35 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental investigation of the aerodynamics of a UAV inlet with double 90° bends;Aerospace Science and Technology;2024-11

2. Experimental Study of the Aerodynamic Performance and Flow Characteristics of an Integrated UAV Inlet with Double 90° Bends;Aerospace;2024-07-21

3. Experimental investigation of a Y-shaped engine inlet at subsonic flow conditions;The Aeronautical Journal;2024-04-24

4. Aerodynamic Instabilities in High-Speed Air Intakes and Their Role in Propulsion System Integration;Aerospace;2024-01-12

5. Seeding-free inlet flow distortion measurements using filtered Rayleigh scattering: integration in a complex intake test facility;AIAA SCITECH 2024 Forum;2024-01-04