Investigation of a two-dimensional scramjet inlet, freestream M = 8-18 and T0 = 4100 K-Reference-Cited by-同舟云学术

Investigation of a two-dimensional scramjet inlet, freestream M = 8-18 and T0 = 4100 K

Published:1993-01 Issue:1 Volume:9 Page:139-145
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Minucci M. A. S.¹,Nagamatsu H. T.²

Affiliation:

1. Institute de Estudos Avancados—CTA, Sao Jose dos Campos, SP 12231-970, Brazil

2. Rensselaer Polytechnic Institute, Troy, New York 12180

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.11496

Reference20 articles.

1. Experimental study of a two-dimensional scramjet inset, M(freestream) = 10.1-25.1

2. 4Minucci, M. A. S. "An Experimental Investigation of a 2-D Scramjet Inlet at Flow Mach Numbers of 8 to 25 and Stagnation Temperatures of 800 to 4,100 K," Ph.D. Dissertation, Rensselaer Polytechnic Inst., Troy,NY, Aug. 1991.

Cited by 13 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. On the unsteady throttling dynamics and scaling analysis in a typical hypersonic inlet–isolator flow;Physics of Fluids;2020-12-01

2. Effects of Mach Number on Non-Rankine–Hugoniot Shock Zone of Mach Reflection;Journal of Spacecraft and Rockets;2019-05

3. Method for Visualizing Viscous Interaction in Hypersonic Low-Density Flows Using Electrical Discharge;Journal of Spacecraft and Rockets;2017-01

4. Rarefaction Effect on the Aerodynamic Performance of Scramjet Inlet in Hypersonic Flow;J AERONAUT ASTRONAUT;2015

5. Numerical analysis of the step jump structure of a scramjet flow by the DSMC method;Journal of the Chinese Institute of Engineers;2013-11-05