Add to ORKGhttp://deepblue.lib.umich.edu/bitstream/2027.42/5033/5/acw3899.0001.001.pdfhttp://deepblue.lib.umich.edu/bitstream/2027.42/5033/4/acw3899.0001.001.tx
"June 1, 1951."Includes bibliographical references (pages 11-12).Office of Naval Research Contract ;...
Cover title."May 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mech...
The computational fluid dynamics method is introduced to study the dynamic response of pressure tran...
"Project M720-4. U. S. Navy Department. Office of Naval Research contract no. N6-ONR-232, Task order...
PhDPhysicsUniversity of Michigan, Horace H. Rackham School of Graduate Studieshttp://deepblue.lib.um...
The purpose of building a shock tube was to give the University another research tool and demonstrat...
An investigation of the AFIT high pressure shock tube was conducted to determine how closely it foll...
A shock tube is proposed in which the flow conditions between the shock wave and advancing interface...
Two shock tubes have been developed which allow for partial or full immersion of the test sections w...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
http://deepblue.lib.umich.edu/bitstream/2027.42/4337/5/bad5127.0001.001.pdfhttp://deepblue.lib.umich...
Shock tubes are devices which are used in the investigation of high speed and high temperature flow ...
Shock tube experiments are a cornerstone of investigations into the hypersonic flight environment. H...
Thesis: Mech. E., Massachusetts Institute of Technology, Department of Mechanical Engineering, 1979I...
Shock tube experiments are a primary means of obtaining ground test data for the hypersonic regime. ...
"June 1, 1951."Includes bibliographical references (pages 11-12).Office of Naval Research Contract ;...
Cover title."May 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mech...
The computational fluid dynamics method is introduced to study the dynamic response of pressure tran...
"Project M720-4. U. S. Navy Department. Office of Naval Research contract no. N6-ONR-232, Task order...
PhDPhysicsUniversity of Michigan, Horace H. Rackham School of Graduate Studieshttp://deepblue.lib.um...
The purpose of building a shock tube was to give the University another research tool and demonstrat...
An investigation of the AFIT high pressure shock tube was conducted to determine how closely it foll...
A shock tube is proposed in which the flow conditions between the shock wave and advancing interface...
Two shock tubes have been developed which allow for partial or full immersion of the test sections w...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
http://deepblue.lib.umich.edu/bitstream/2027.42/4337/5/bad5127.0001.001.pdfhttp://deepblue.lib.umich...
Shock tubes are devices which are used in the investigation of high speed and high temperature flow ...
Shock tube experiments are a cornerstone of investigations into the hypersonic flight environment. H...
Thesis: Mech. E., Massachusetts Institute of Technology, Department of Mechanical Engineering, 1979I...
Shock tube experiments are a primary means of obtaining ground test data for the hypersonic regime. ...
"June 1, 1951."Includes bibliographical references (pages 11-12).Office of Naval Research Contract ;...
Cover title."May 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mech...
The computational fluid dynamics method is introduced to study the dynamic response of pressure tran...