Design and Wind Tunnel Study of a Top-mounted Diverterless Inlet-Reference-Cited by-同舟云学术

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Design and Wind Tunnel Study of a Top-mounted Diverterless Inlet

Published:2004-05 Issue:2 Volume:17 Page:72-78
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

TAN Hui-jun,GUO Rong-wei

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference6 articles.

1. Simon P C, Brown D W, Huff R G. Performance of external-compression bump inlet at Mach numbers of 1.5 to 2.0[R]. NACA RM E56L19, 1957.

2. Lee C C, Boekicker C. Subsonic diffuser design and performance for advanced fighter aircraft [R], AIAA-85-3073, 1985.

3. Richard J R. An investigation of several NACA-series inlets at Mach number from 0.4 to 1.29 for mass-flow ratio near 1.0 [R]. NASA TM-X-3324, 1975.

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2. Numerical Simulation of a Y-Shaped Diverterless Supersonic Inlet;Journal of Aircraft;2023-07

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