Test Time in a 1.5-Inch-Diameter High-Stagnation-Enthalpy Shock Tube

AIAA Journal ◽  
1963 ◽  
Vol 1 (5) ◽  
pp. 1236-1237
Author(s):  
V. A. SANDBORN ◽  
H. WEISBLATT ◽  
R. F. FLAGG
Keyword(s):  
Shock Tube ◽  
Test Time ◽  
Stagnation Enthalpy

scholarly journals Measurements of test time in the galcit 17-inch shock tube

AIAA Journal ◽  
1964 ◽  
Vol 2 (1) ◽  
pp. 186-187 ◽  
Author(s):  
ANATOL ROSHKO ◽  
JEROME A. SMITH
Keyword(s):  
Shock Tube ◽  
Test Time

Influence of turbulent boundary layer on shock tube test time

AIAA Journal ◽  
1965 ◽  
Vol 3 (5) ◽  
pp. 960-961
Author(s):  
PETER JEANMAIRE ◽  
ERIC F. BROCKER
Keyword(s):  
Boundary Layer ◽  
Turbulent Boundary Layer ◽  
Shock Tube ◽  
Test Time ◽  
Tube Test ◽  
Shock Tube Test

Series solutions for shock tube laminar boundary layer and test time.

AIAA Journal ◽  
1966 ◽  
Vol 4 (5) ◽  
pp. 782-789 ◽  
Author(s):  
HAROLD MIRELS ◽  
WILLIAM S. KING
Keyword(s):  
Boundary Layer ◽  
Shock Tube ◽  
Laminar Boundary Layer ◽  
Test Time ◽  
Series Solutions

Test Time Determination by End Wall Pressure Measurement in an Arc-Driven Shock Tube

AIAA Journal ◽  
1975 ◽  
Vol 13 (2) ◽  
pp. 255-256
Author(s):  
A. J. MULAC ◽  
J. L. MARK ◽  
J. A. GUZMAK
Keyword(s):  
Shock Tube ◽  
Pressure Measurement ◽  
Wall Pressure ◽  
Test Time ◽  
Time Determination ◽  
End Wall

Stagnation Point Heat Transfer Measurements at Super Satellite Speeds

1962 ◽  
Vol 66 (613) ◽  
pp. 53-53 ◽  
Author(s):  
E. Offenhartz ◽  
H. Weisblatt ◽  
R. F. Flagg
Keyword(s):  
Heat Transfer ◽  
Experimental Data ◽  
Heat Conduction ◽  
Shock Tube ◽  
Stagnation Point ◽  
Blunt Body ◽  
Foot Length ◽  
Electronic Heat ◽  
Series Of Experiments ◽  
Stagnation Enthalpy

Recent lunar and planetary return vehicle studies have stimulated interest concerning the effect upon stagnation point heating due to electronic heat conduction associated with re-entry at speeds greater than 30,000 ft./sec. In order to provide experimental data for comparison with theory, a series of experiments was undertaken in which shock tube techniques were utilised for the measurement of the stagnation point heating of a blunt body over a stagnation enthalpy (Hst/RT0) range of 650 to 900, corresponding to velocities between 32,000 ft./sec. and 39,000 ft. /sec. respectively. The tests were performed in a 1·5 inch diameter shock tube with 3 foot length driver and 16 foot length driven section.

On determination of test time in a shock tube

2008 ◽  
Vol 51 (5) ◽  
pp. 748-752
Author(s):  
A. S. Chizhikov
Keyword(s):  
Shock Tube ◽  
Test Time

A New-Conception, Electromagnetically Controlled, Diaphragmless Shock Tube

2003 ◽  
Author(s):  
Giovanni Ferrara ◽  
Lorenzo Ferrari ◽  
Maurizio De Lucia
Keyword(s):  
Shock Wave ◽  
Mach Number ◽  
Shock Tube ◽  
Test Time ◽  
Shock Formation ◽  
Test Results ◽  
Diaphragmless Shock Tube ◽  
Two Factors ◽  
University Of Florence ◽  
Contact Sensors

A new conception, electro-magnetically controlled, diaphragmless shock tube was realized and tested in the laboratories of University of Florence. A piston separates the co-axial driver and driven sections. The piston is kept in position by a force of an electromagnet acting on an iron disc linked to its rod. In order to obtain very short opening time, light materials were tested for moving devices: aluminum, ergal, titanium and iron. Opening time was measured using contact sensors. Several different dimensionless driven section lengths were tested by changing the driven section length and by reducing the driven section diameter. The influence of the two factors on shock presence and shock formation was analyzed separately. Tests were carried out for driver-to-driven pressure ratios of up to 22, obtaining shock waves at Mach number of up to 1.70 with a difference from the theoretical value for a straight shock tube of 9%. A configuration for increasing the useful test time after the shock passage is also proposed and tested. The system realized is simple, easy-to-use, quite cheap and can be a very useful way of obtaining a reproducible shock wave. The shock tube details and the test results are reported below.

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