Parametric Analysis and Design for Embedded Engine Inlets-Reference-Cited by-同舟云学术

Parametric Analysis and Design for Embedded Engine Inlets

Published:2015-05 Issue:3 Volume:31 Page:843-850
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Florea Razvan V.¹,Matalanis Claude¹,Hardin Larry W.¹,Stucky Mark¹,Shabbir Aamir¹

Affiliation:

1. Thermal and Fluid Sciences, United Technologies Research Center, East Hartford, Connecticut 06108

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34804

Reference13 articles.

1. Aircraft System Study of Boundary Layer Ingesting Propulsion

2. Performance of a Boundary Layer Ingesting (BLI) Propulsion System

3. DaggettD. L.KawaiR.FriedmanD. “Blended Wing Body Systems Studies: Boundary Layer Ingestion Inlets with Active Flow Control,” NASA CR-2003-212670, Dec. 2003.

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

5. Hybrid Wing Body Configuration System Studies

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