Abstract
This paper describes a unique device that has been developed for the transient loading of models along straight and curved boundaries and that operates by discharge of a high-energy, high-voltage capacitor bank. In its present configuration, this device can generate uniform pressures from 1500 psi (10 MPa) to pressures that approach 100,000 psi (690 MPa) and that rise from zero to maximum pressure in 2 μs and decay to approximately zero in another 2 μs.
The transient stress-wave patterns in photoelastic models loaded with this device have been recorded by a dynamic polariscope. The dynamic polariscope presently in use is identical to a static polariscope except that the light source is of a short enough duration (½ μs) to photographically stop the movement of the photoelastic-fringe patterns caused by the stress wave.
With the stress-wave generator and the dynamic polariscope, transient photoelastic patterns have been recorded in a number of models. These patterns indicate that the scatter from duplicate shots performed with this technique is on the order of 3 percent. This represents considerable improvement over the 15-percent scatter normally experienced with sheet-explosive loading techniques. This improvement and the rapid turnaround between shots (approximately 5 min) are distinct advantages this system has over other methods of dynamic loading.
Similar content being viewed by others
Abbreviations
- a :
-
integration constant
- b :
-
integration constant
- C :
-
capacitance (μF)
- c :
-
phase velocity (mm/μs)
- c o :
-
elastic propagation velocity for dilatational wave in a flat plate (mm/μs)
- I max :
-
maximum current (A)
- i(t) :
-
current as a function of time (A)
- L :
-
inductance (H)
- m 1,2 :
-
\( - \frac{R}{{2L}} \pm \sqrt {\left( {\frac{R}{{2L}}} \right)^2 - \frac{1}{{LC}}(s^{ - 1} )} \)
- N :
-
resolution of polariscope system (fringes/mm)
- P :
-
pressure (Pa or psi)
- Q o :
-
initial charge (C)
- Q(t) :
-
charge as a function of time (C)
- R :
-
resistance (Ω)
- S :
-
dimensionless proportionality constant
- T :
-
period of oscillation (μs)
- t :
-
instantaneous time
- t e :
-
duration of light source (μs)
- V o :
-
initial voltage (V)
- W :
-
width of loading strips (m)
- A 3/A 1 :
-
inverse ratio of successive peaks of the same polarity
- α:
-
R/2L (Ω/H)
- β:
-
magnetic intensity (Wb/m2)
- γ:
-
Taylor series coefficient of the expansion of phase velocityc in frequency ω (m·s)
- ε y :
-
strain in the plane of the sample perpendicular to the stress-wave propagation direction (μin./in. or μm/m)
- μ:
-
magnetic permeability (4π×10−7 Wb/A·m2)
- ω:
-
frequency (rad/s)
- Ω:
-
circular frequency\(\sqrt {\frac{1}{{LC}} - \left( {\frac{R}{{2L}}} \right)^2 } (rad/s)\)
References
Okada, A., Cunningham, D. M. andGoldsmith, W., “Stress Waves in Pyramids by Photoelasticity,”Experimental Mechanics,8 (7),289–299 (1968).
Brillhart, L. V. andDally, J. W., “A Dynamic Photoelastic Investigation of Stress-wave Propagation in Cones,”Experimental Mechanics,8 (7),145–153 (1968).
Rose, J. L. andChou, P. C., “Study of Cylindrical Stress Waves Generated by Exploding Wires,”Experimental Mechanics,12 (2),104–106 (1972).
Rose, J. L. andChou, P. C., “Elastic Stress Waves in Layered Composite Materials,”J. of Comp. Mat.,5,405–407 (July 1971).
Hoffman, O., et al., “Study of Advanced Filament-Reinforced Composite Materials-Final Report,”Defense Atomic Support Agency, Washington, DC, 123–160 (April 1970).
Meagher, T. F. V. and Williams, D. C., “The Theory and Capabilities of Magnetically Driven Flyers,” Defense Atomic Support Agency, DASA-2440 (June 1970).
Ibid. Meagher, T. F. V. and Williams, D. C., “The Theory and Capabilities of Magnetically Driven Flyers,” Defense Atomic Support Agency, 10.
Chern, D. C. andKorneff, T., “Current Distribution for Wire Exploded in Vacuo,”Exploding Wires,4,ed. by W. G. Chace andH. K. Moore,Plenum Press,New York,173–183 (1968).
Dally, J. W., Henzi, A. and Lewis, D., “On the Fidelity of High-Speed Photographic Systems for Dynamic Photoelasticity,” presented at SESA Spring Meeting, Philadelphia, PA (May 13–16, 1969).
Honnold, V. R., Berggren, C. C. andPeffley, W. M., “Investigation of Dynamic Mechanical Stress With Photoelastic Techniques,”Air Force Weapons Laboratory, AFWL-TR-69-154, Kirtland AFB, NM (April 1970).
Riley, W. F. andDally, J. W., “A Photoelastic Analysis of Stress-Wave Propagation in a Layered Model,”J. of Geophysics,XXXI (5),881–889 (Oct. 1966).
Reynolds, R. W. and Jacobson, R. S., “Numerical Prediction of the Motion of Magnetically Accelerated Flyer Plates,” Sandia Laboratories, SCL-DR-69-44 (July 1969).
Pottinger, M. G., “Gage Length Effects on Strain Measurements,” Instruments and Controls, 115–116 (Sept. 1970).
Kolsky, H., “Stress Waves in Solids,”Clarendon Press, Oxford (1953);79–81, Dover Reprint (1963).
Peck, J. C., “Pulse Attenuation in Composites,” Shock Waves and the Mechanical Properties of Solids, ed. by J. J. Burke and Z. Weiss, Syracuse Press (1971).
Maiden, C. J. and Green, S. G., “Compressive Strain-Rate Tests on Six Selected Materials at Strain Rates From 10 −3 to 10 −4 in/in/sec.,” Trans. ASME, Series E, J. of Appl. Mech., 496–504 (Sept. 1966).
Achenbach, J. D., “An Asymptotic Method to Analyze the Vibrations of an Elastic Layer,” J. of Appl. Mech., 65–72 (Mar. 1969).
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Snell, R.F., MacKallor, D.C. & Guernsey, R. An electromagnetic, plane stress-wave generator. Experimental Mechanics 13, 472–479 (1973). https://doi.org/10.1007/BF02322733
Received:
Revised:
Issue Date:
DOI: https://doi.org/10.1007/BF02322733