Submerged Inlet Performance Enhancement Using a Unique Bump-Shaped Vortex Generator-Reference-Cited by-同舟云学术

Submerged Inlet Performance Enhancement Using a Unique Bump-Shaped Vortex Generator

Published:2016-09 Issue:5 Volume:32 Page:1275-1280
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Sun Shu¹,Tan Hui-Jun¹,Wang Chen-Xi¹

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, Nanjing 210016, People’s Republic of China

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.B36085

Reference29 articles.

1. Inlet and Nozzle Technology for 21st Century Fighter Aircraft

2. FrickC. W.DavisW. F. “An Experimental Investigation of NACA Submerged-Duct Entrances,” NACA ACR-5120, California, 1945.

3. MossmanE. A.GaultD. E. “Development of NACA Submerged Inlets and Comparison with Wing Leading-Edge Inlets for 1/4-Scale Model of a Fighter Airplane,” NACA RM-A7A31, California, 1947.

4. RandalL. M.MossmanE. A. “An Experimental Investigation of the Design Variables for NACA,” NACA RM-A7130, California, 1948.

5. DelanyN. K. “An Investigation of Submerged Air Inlets on a 1/4-Scale Model of a Typical Fighter-Type Airplane,” NACA RM-A8A20, California, 1948.

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