Investigation of shock dynamics in an axisymmetric inlet/isolator with attached boundary layers-Reference-Cited by-同舟云学术

Investigation of shock dynamics in an axisymmetric inlet/isolator with attached boundary layers

Published:2020-12-15 Issue: Volume:908 Page:
ISSN:0022-1120
Container-title:Journal of Fluid Mechanics
language:en
Short-container-title:J. Fluid Mech.

Author:

Leonard Michael D.,Narayanaswamy V.^ORCID

Abstract

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference25 articles.

1. Curran, E. T. & Stull, F. E. 1964 The utilization of supersonic combustion ramjet systems at low Mach numbers. Tech Rep. RTD-TDR-63-4097. Aero Propulsion Lab.

2. Numerical Investigation of Shock-Train Response to Inflow Boundary-Layer Variations

3. The Mechanism of Pseudo-Shock Waves

4. Miller, J. H. 2018 Pressure scalings and influence region research. Tech Rep. AFRL Tech Briefs.

5. VIBRATION OF PSEUDO-SHOCK IN STRAIGHT DUCT : 1ST REPORT, FLUCTUATION OF STATIC PRESSURE

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