Search results (Open Library)

Search Results

There are 55 matching records. Show: List / Covers

	Design of transient discharge arc-driven shock tubes by B. E. Milton School of Mechanical and Industrial Engineering, University of New South Wales, 1987
	Shock tubes by I. I. Glass Institute of Aerophysics, 1958
	Open ended shock tube flow as a tool to aid development of a two-dimensional compressible nonsteady computer code by E. G. Plett AIAA, 1986
	The design and applications of a new aerodynamic range by W. B. Fallis Dept. of Aeronautical Engineering, University of Toronto, 1950
	Research on a facility for the study of shock and expansion wave flows at extreme physical conditions by A. G. Boyer [Institute for Aerospace Studies], 1965
	A theoretical and experimental study of the shock tube by I. I. Glass Institute of Aerophysics, 1953
	On the length of a shock tube by R. Kenneth Lobb Institute of Aerophysics, 1950
	Analytical and numerical study of the flow in a shock tube with an area change at the diaphragm section by Hema Sandhyarani Murty Dept. of Aerospace Science and Engineering, 1983
	Design and performance of shock tubes by C. I. H. Nicholl Institute of Aerophysics, University of Toronto, 1949
	Design and construction of a shock tube by Domenic Bitondo Institute of Aerophysics, 1950
	Shock Tube Research University of Toronto Press, June 1971 Hardcover
	Shock tubes and waves Magnes Press, 1980 Unknown Binding
	The study of supersonic flows in a shock tube. by Rodmond Kenneth Lobb 1950
	Simulation of a travelling sonic boom in a pyramidal horn by James Joseph Gottlieb s.n.], 1974
	An analytical and experimental study of an implosion-driven shock tube by Sek-kwan Chan 1973
	A magnetohydrodynamic flow in the shock tube boundary layer with transverse magnetic field. by Janusz Karol Dukowicz 1966
	Shock tubes. Part II by J. Gordon Hall Institute of Aerophysics, 1958
	Beyond three decades of continuous research at UTIAS on shock tubes and waves by I. I. Glass Institute for Aerospace Studies, 1981
	Pitot-pressure measurements in the nozzle of the UTIAS 11" x 15" hypersonic shock tunnel by R. P. Mason [Institute for Aerospace Studies], 1965
	The design of a wave interaction tube by I. I. Glass Institute for Aerophysics, 1950

More results: 1 2 3 NEXT >

Can't find the book you are searching for? Add a new book.

Search = 0.18 sec; Presentation = 0.00 sec

There are 55 matching records. Show: List / Covers

full text

authors

subjects

publication date

languages

publishers