External-Compression Supersonic Inlet Free from Violent Buzz-Reference-Cited by-同舟云学术

External-Compression Supersonic Inlet Free from Violent Buzz

Published:2019-06 Issue:6 Volume:57 Page:2513-2523
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Chen Hao¹,Tan Hui-jun¹,Liu Ya-zhou¹,Zhang Qi-fan²

Affiliation:

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

2. Chinese Academy of Sciences, 100190 Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

Jiangsu Province “333” Project

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057811

Reference40 articles.

1. OswatitschK. “Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds,” NACA TM-1140, 1947.

2. Intake Aerodynamics, Second Edition

3. Aircraft Propulsion Systems Technology and Design

4. DaileyC. L. “Supersonic Diffuser Instability,” Ph.D. Dissertation, California Inst. of Technology, Pasadena, CA, 1954.

5. FisherS. A.NealeM. C.BrooksA. J. “On the Sub-Critical Stability of Variable Ramp Intakes at Mach Numbers Around 2,” National Gas Turbine Establishment Rept. ARC-R/M-3711, Fleet, England, U.K. Feb. 1972.

Cited by 18 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. A review on aero-engine inlet-compressor integration and inlet flow distortion in axial compressors;Fundamental Research;2024-04

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

3. Experimental investigation on unstart-restart hysteresis of a supersonic inlet during throat regulation;Chinese Journal of Aeronautics;2023-11

4. Source of buzz instability in a supersonic air inlet;Aerospace Science and Technology;2023-07

5. Unstart/Restart Boundary Broadening Method for a Two-Dimensional Supersonic Variable Inlet Based on a Distributed Bleed System;Journal of Aerospace Engineering;2023-01