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Shock tube
An Engine and Shock Tube Study in Combustion Soot Measurement By
Absolute Radiation Measurement During Planetary Entry in the NASA Ames Electric Arc Shock Tube Facility
The Design and Implementation of a Supersonic Indraft Tube Wind Tunnel for the Demonstration of Supersonic Flows
The Design and Construction of a Shock Tube Facility
Computational Challenges for Simulations Related to the NASA Electric Arc Shock Tube (EAST) Experiments Dmitry V
Driver-Gas Tailoring for Test-Time Extension Using Unconventional Driver Mixtures
An Improved Hydrogen/Oxygen Mechanism Based on Shock Tube/Laser Absorption Measurements
The Combustion Driven Shock Tube Ae 104C Final Report
Shock Tube and Ballistic Range Facilities at NASA Ames Research Center
Kinetics of Methyl Iodide-Iodine Exchange in a Shock Tube Allen Jay Kassman Iowa State University
Hypersonic Wind Tunnel
Shock Tube Studies of Kinetics of Conventional and Alternative Engine Fuels
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