Experimental Investigation of a Fixed-geometry Two-dimensional Mixed-compression Supersonic Inlet with Sweep-forward High- light and Bleed Slot in an Inverted “X”-type Layout-Reference-Cited by-同舟云学术

Experimental Investigation of a Fixed-geometry Two-dimensional Mixed-compression Supersonic Inlet with Sweep-forward High- light and Bleed Slot in an Inverted “X”-type Layout

Published:2007-08 Issue:4 Volume:20 Page:304-312
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Wan Dawei,Guo Rongwei

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference8 articles.

1. Practical intake aerodynamic design;Goldsmith,1993

2. Syberg J, Koncsek L. Bleed system design technology for supersonic inlets. AIAA 72–1138, 1972.

3. Murakami A, Yanagi R. Mach 3 wind tunnel test of mixed compression supersonic inlet. AIAA 92-3625, 1992.

4. Gary J, Gregory, E. On supersonic-inlet boundary-layer bleed flow. AIAA 95-0038, 1995.

5. Numerical simulation and experimental validation of the flow in a mixed-compression axisymmetric supersonic inlet with fixed-geometry;Xie;Acta Aeronautica et Astronautica Sinica,2007

Cited by 8 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. Flow Field Investigation of a Rectangular Supersonic Air-Intake With Cowl Bending;Journal of Aerospace Sciences and Technologies;2023-08-07

2. Throttling Characteristics of a Supersonic Variable Inlet at Different Internal Contraction Ratios;AIAA Journal;2022-09

3. Parameters for evaluating the efficiency of inlet compression;Chinese Journal of Aeronautics;2021-12

4. Evolution of turbulent boundary layer over a three-dimensional bump;Chinese Journal of Aeronautics;2021-11

5. Numerical Simulation of Supersonic Flow through Scramjet Intake with Concavity in Cowl Surface;Journal of Applied Fluid Mechanics;2020-09-01