HyperTERP: A newly commissioned hypersonic shock tunnel at the University of Maryland-Reference-Cited by-同舟云学术

HyperTERP: A newly commissioned hypersonic shock tunnel at the University of Maryland

Published:2019-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Aviation 2019 Forum
language:
Short-container-title:

Author:

Butler Cameron¹,Laurence Stuart J.¹

Affiliation:

1. University of Maryland, College Park

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. Pennelegion, L. and Gough, P. “The Change in Shock-Tunnel Tailoring Mach Number Due to Driver Gas Mixtures of Helium and Nitrogen,” Tech. Rep. 3398, Ministry of Aviation, 1963.

2. Ames Research Staff, “Equations, tables, and charts for compressible flow,” NACA Report 1135, 1953.

3. White, J. and Morrison, J. “A Pseudo-Temporal Multi-Grid Relaxation Scheme for Solving the Parabolized Navier-Stokes Equations,” Tech. Rep. 99-3360, AIAA, 1999.

Cited by 12 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. Attenuation of the acoustic noise radiated by a compressible boundary layer through injection of a vibrationally active gas;Experiments in Fluids;2024-01-27

2. Laser Absorption Sensor Targeting Potassium for Hypersonic Velocity, Temperature, and Enthalpy Measurements;AIAA Journal;2023-08

3. Hypersonic Boundary-Layer Disturbances on a Cooled, Slender Cone at Mach 6;Journal of Spacecraft and Rockets;2023-03

4. A multi-point focused laser differential interferometer for characterizing freestream disturbances in hypersonic wind tunnels;Experiments in Fluids;2022-11

5. Transitional hypersonic flow over slender cone/flare geometries;Journal of Fluid Mechanics;2022-09-30