Analytical method of evaluating nonuniformities in shock tube flows: application
Shock tube experiments are a primary means of obtaining ground test data for the hypersonic regime. Accurate characterization of the test gas is crucial to understanding experimental results. However, characterization of the flows produced behind the shock wave has historically proven challenging. T...
Main Authors: | Satchell, M, Glenn, A, Collen, P, Penty-Geraets, R, McGilvray, M, Di Mare, L |
---|---|
Format: | Journal article |
Language: | English |
Published: |
American Institute of Aeronautics and Astronautics
2021
|
Similar Items
-
Analytical method of evaluating nonuniformities in shock tube flows: theory and development
by: Satchell, M, et al.
Published: (2021) -
Analysis of shock deceleration effects in the NASA electric arc shock tube
by: Collen, PL, et al.
Published: (2023) -
Emission spectroscopy of low density air shock tube flows above 10 km/s
by: Hermann, T, et al.
Published: (2022) -
The influence of shock speed variation on radiation and thermochemistry experiments in shock tubes
by: Cone, PL, et al.
Published: (2022) -
Numerical model for non-equilibrium shock tube flow
by: Clarke, JP, et al.
Published: (2022)