AN EXPERIMENTAL INVESTIGATION OF NONEQUILIBRIUM CORNER EXPANSION FLOWS OFDISSOCIATED OXYGEN GENERATED IN A GLOW DISCHARGE SHOCK TUBE
Main Author: | SUSTEK, ALVIN JOHN, JR. |
---|---|
Format: | Others |
Language: | English |
Published: |
2007
|
Subjects: | |
Online Access: | http://hdl.handle.net/1911/14798 |
Similar Items
-
The Characterization and Feasibility of a Low-Duty-Cycle Diaphragmless Shock Tube
by: Taylor, David Christopher
Published: (2012) -
Experimental Study of Fillets to Reduce Corner Effects in an Oblique Shock-Wave/Boundary-Layer Interaction
by: Hirt, Stefanie M.
Published: (2015) -
Curved aerodynamic shock waves
by: Molder, Sannu
Published: (2012) -
Oxygen glow discharge treatment in terms of hardness coating
by: HUI-CHU CHEN, et al.
Published: (2006) -
Analysis of shock dynamics in supersonic intakes
by: Tahir, Råbi
Published: (2009)