Author:
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Category :
Languages : en
Pages :
Book Description
Proceedings of the Fourth Shock Tube Symposium Sponsored by the Ballistic Research Laboratory 18-20 April 1961
Author:
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Category :
Languages : en
Pages :
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Publisher:
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Category :
Languages : en
Pages :
Book Description
Proceedings of the Fourth Shock Tube Symposium, 18 - 20 April 1961, Aberdeen Proving Ground, Maryland
Author:
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Category : Aerodynamics, Hypersonic
Languages : en
Pages : 476
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 476
Book Description
Proceedings of the 4th Shock Tube Symposium
Author:
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Category :
Languages : en
Pages :
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Category :
Languages : en
Pages :
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Proceedings of the Fourth International Shock Tube Symposium
Author: U.S. Army Ballistic Research Laboratory
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Category : Shock tubes
Languages : en
Pages : 952
Book Description
Publisher:
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Category : Shock tubes
Languages : en
Pages : 952
Book Description
PROCEEDINGS OF THE FOURTH SHOCK TUBE SYMPOSIUM 18-20 APRIL 1961
Author:
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Category :
Languages : en
Pages : 393
Book Description
NOL model nuclear airblast simulator The soil filled shock tube A shock tube modified to produce sharp-rising overpressures of 400 milliseconds duration A high explosive operated shock tube with facilities for testing structures Volume detonation in shock tubes High pressure loading device for evaluating blast closure performance Techniques for producing long- duration loads in the NCEL blast simulator Arc heating technique for shock tube driver Pressure and heat-transfer instrumentation used in the NOL hypersonic shock tunnels Measurements in the hypersonic shock tunnel at I.S.L. Shock wave decay in tunnels Republic 24-in hypervelocity wind tunnel.
Publisher:
ISBN:
Category :
Languages : en
Pages : 393
Book Description
NOL model nuclear airblast simulator The soil filled shock tube A shock tube modified to produce sharp-rising overpressures of 400 milliseconds duration A high explosive operated shock tube with facilities for testing structures Volume detonation in shock tubes High pressure loading device for evaluating blast closure performance Techniques for producing long- duration loads in the NCEL blast simulator Arc heating technique for shock tube driver Pressure and heat-transfer instrumentation used in the NOL hypersonic shock tunnels Measurements in the hypersonic shock tunnel at I.S.L. Shock wave decay in tunnels Republic 24-in hypervelocity wind tunnel.
PROCEEDINGS 4TH SHOCK TUBE SYMPOSIUM- BALLISTIC RESEARCH LABORATORIES.
Author:
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Category :
Languages : en
Pages :
Book Description
Publisher:
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Category :
Languages : en
Pages :
Book Description
U.S. Government Research Reports
Author:
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Category : Science
Languages : en
Pages : 1416
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1416
Book Description
Symposia
Author: Defense Documentation Center (U.S.)
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Category : Congresses and conventions
Languages : en
Pages : 290
Book Description
Publisher:
ISBN:
Category : Congresses and conventions
Languages : en
Pages : 290
Book Description
Strain Gage Readings
Author:
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Category : Strain gages
Languages : en
Pages : 754
Book Description
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ISBN:
Category : Strain gages
Languages : en
Pages : 754
Book Description
The Tolerance of Guinea Pigs to Air Blast when Mounted in Shallow, Deep, and Deep-with-offset Chambers on a Shock Tube
Author: Donald R. Richmond
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Category : Blast effect
Languages : en
Pages : 52
Book Description
One hundred and eighteen guinea pigs were exposed to air blast in shallow, deep, and deep-with-offset chambers mounted on a shock tube. The LD(50)- 24 hours, in terms of the incident shock pressures measured adjacent to the chambers, was calculated by probit analysis to be 34.9 psi, 19.5 psi, and 26.8 psi for animals in the shallow, deep, and deep-with-offset chambers, respectively. According to the LD(50) incident pressures, the shallow chambers offered the most protection against air blast; the deep chambers, the least. Comparing the LD(50)pressure dose at the animals' location revealed little difference in their tolerance to overpressure, per se; i.e., LD(50) reflected pressures measured by gauges within the deep and deep-with-offset chambers were 34.6 psi and 35.9 psi, respectively. The LD(50) incident shock pressure of 34.9 psi in the shallow chambers was considered to be the dose at the animal's location in that instance. The protection against blast provided by the three chambers and the response of animals to the particular pressure time patterns encountered are discussed.
Publisher:
ISBN:
Category : Blast effect
Languages : en
Pages : 52
Book Description
One hundred and eighteen guinea pigs were exposed to air blast in shallow, deep, and deep-with-offset chambers mounted on a shock tube. The LD(50)- 24 hours, in terms of the incident shock pressures measured adjacent to the chambers, was calculated by probit analysis to be 34.9 psi, 19.5 psi, and 26.8 psi for animals in the shallow, deep, and deep-with-offset chambers, respectively. According to the LD(50) incident pressures, the shallow chambers offered the most protection against air blast; the deep chambers, the least. Comparing the LD(50)pressure dose at the animals' location revealed little difference in their tolerance to overpressure, per se; i.e., LD(50) reflected pressures measured by gauges within the deep and deep-with-offset chambers were 34.6 psi and 35.9 psi, respectively. The LD(50) incident shock pressure of 34.9 psi in the shallow chambers was considered to be the dose at the animal's location in that instance. The protection against blast provided by the three chambers and the response of animals to the particular pressure time patterns encountered are discussed.