EXPERIMENTS ON NON-EQUILIBRIUM SUPERSONIC FLOW SHOCK STAND-OFF DISTANCE OF SPHERES CARRIED OUT IN A NEW TYPE OF INTERMITTENT WIND TUNNEL

1969 ◽  
Author(s):  
George Buzyna ◽  
Peter P. Wegener
Keyword(s):  
Supersonic Flow ◽  
Wind Tunnel ◽  
New Type ◽  
Non Equilibrium

Wind tunnel interference on oscillating airfoils in low supersonic flow

1973 ◽  
Vol 16 (1-2) ◽  
pp. 115-126
Author(s):  
M. F. Platzer
Keyword(s):  
Supersonic Flow ◽  
Wind Tunnel

scholarly journals A New Type of Radiometric Analysis—Non-equilibrium Isotopic Exchange Method

RADIOISOTOPES ◽  
1969 ◽  
Vol 18 (6) ◽  
pp. 224-226 ◽  
Author(s):  
Nagao IKEDA ◽  
Kan KIMURA ◽  
Yasuko TAKAHASHI ◽  
Yoshiko FUJIKI
Keyword(s):  
Isotopic Exchange ◽  
Exchange Method ◽  
Radiometric Analysis ◽  
New Type ◽  
Non Equilibrium

Calculation of the Flow Properties Up- and Downstream of and Within a Supersonic Turbine Cascade

1972 ◽  
Author(s):  
O. K. Lawaczeck
Keyword(s):  
Supersonic Flow ◽  
Wind Tunnel ◽  
Pressure Distribution ◽  
Theoretical Method ◽  
Experimental Results ◽  
Turbine Cascade ◽  
Flow Properties ◽  
Flow Through

This paper deals with the flow through cascades, which have a supersonic flow up- and downstream. A theoretical method is described to calculate, under certain conditions, the flow quantities up- and downstream of and within the cascade and to determine the pressure distribution on the blades. The method is compared with experimental results, carried out in the cascade wind tunnel of the Aero dynamische Versuchsanstalt Göttingen (AVA), Germany.

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