Flow Characteristics of an Ultracompact Serpentine Inlet with an Internal Bump-Reference-Cited by-同舟云学术

Flow Characteristics of an Ultracompact Serpentine Inlet with an Internal Bump

Published:2018-03 Issue:2 Volume:31 Page:04017089
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sun Shu¹,Tan Hui-jun²

Affiliation:

1. Associate Professor, College of Civil Aviation, Nanjing Univ. of Aeronautics and Astronautics, No. 29 Jiangjun Rd., Nanjing 211106, People’s Republic of China.

2. Professor, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, No. 29 Yudao St., Nanjing 210016, People’s Republic of China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000801

Reference23 articles.

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2. Flow Separation Within the Engine Inlet of an Uninhabited Combat Air Vehicle (UCAV)

3. The Swirl in an S-Duct of Typical Air Intake Proportions

4. Active inlet flow control technology demonstration;Hamstra J. W.;Aeronaut. J.,2016

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