Abstract
True membranes are no-compression structures which exhibit the unique response of wrinkling. Prediction of the associated wrinkle parameters is of practical importance. Accurate measurement of membrane wrinkling has heretofore not been presented in the literature; among other requirements, noncontact methods must be used. First, some background information on membrane wrinkling prediction and measurement is given. Then, an experimental apparatus is discussed within which a membrane was subject to planar loading. The measurement system consisted of a capacitance-based noncontact displacement sensor mounted in anXYZ frame. A computer controlled the forces applied to the membrane, as well as the motion of theXYZ frame during data acquisition. Results are presented and conclusions are drawn regarding the wrinkle parameters.
Similar content being viewed by others
References
Jenkins, C.H. andLeonard, J.W., “Nonlinear Dynamic Response of Membranes: State of the Art,”Appl. Mech. Rev.,44,319–328 (1990).
Jenkins, C.H., “Nonlinear Dynamic Response of Membranes: State of the Art—Update,”Appl. Mech. Rev.,49 (10),S41-S49 (1996).
Jenkins, C.H. andLeonard, J.W., “Dynamic Wrinkling of Viscoelastic Membranes,”J. Appl. Mech.,60,575–582 (1993).
Wagner, H., “Flat Sheet Girder with Very Thin Metal Web,”Z. Flugtech. Motorluft-Schiffahrt,20,200–207,227–231, 281–284, 306–314 (1929).(Reprinted as NACA Technical Memorandum 604–606, NACA, Washington, DC, 1931.)
Lilly, W.E., Engineering (February 1, 1907).
Southwell, R.V. and Skan, S.W., “On the Stability Under Shearing Forces of a Flat Elastic Strip, Proc. Roy. Soc. A,105,582–607.
Kuhn, P., Stresses in Aircraft and Shell Structures, McGraw-Hill, New York (1956).
Stein, M. and Hedgepeth, J.M., “Analysis of Partly Wrinkled Membranes,” NASA Technical Note D-813, Washington, DC (1961).
Mikulas, M.M., “Behavior of a Flat Stretched Membrane Wrinkled by the Rotation of an Attached Hub,” NASA Technical Note D-2456, Washington, DC (1964).
Leonard, R.W., Brooks, G.W., and McComb, H.G., “Structural Considerations of Inflatable Reentry Vehicles,” NASA Technical Note D-457, Washington, DC (1960).
Mansfield, E.H., “Load Transfer via a Wrinkled Membrane,”Proc. Roy. Soc. Lon. Ser. A,316,269–289 (1970).
Szyszkowski, W. andGlockner, G., “Spherical Membranes Subjected to Vertical Concentrated Loads: An Experimental Study,”Eng. Struct.,9,183–192 (1987).
Broderick, L. andJenkins, C.H., “Experimental Investigation of a Fluid-filled Membrane Breakwater,”J. Waterway Port Coastal Ocean Eng.,119,639–656 (1993).
Schur, W.W., “Development of a Practical Tension Field Material Model for Thin Films,” 32nd Aerospace Sciences Meeting and Exposition, Reno, NV, AIAA 94-0636 (1994).
Pereira, P. andZheng, Y.F., “Sensing Strategy to Detect Wrinkles in Components,”IEEE Trans. Instrumentation Meas.,43,442–448 (1994).
Haugen, F., “Control of Membrane Wrinkling: Advanced Numerical and Experimental Investigation,”M.S. thesis, South Dakota School of Mines and Technology, Rapid City (1996).
Jenkins, C.H., Spicher, W.H., and Vedoy, A., “Evaluation of Membrane Wrinkling by Noncontact Measurement,” Proc. 24th Midwestern Mechanics Conf., Ames, IA (1995).
Jenkins, C.H., Spicher, W.H., and Vedoy, A., “Experimental Measurement of Wrinkling in Plane Elastic Sheets,” Proc. 1996 Spring Conf. Society of Experimental Mechanics, Nashville, TN (1996).
Jenkins, C.H. and Najdawi, H.F., “Wrinkle Prediction and Measurement in Planar Deformations of Finite Elastic Sheets,” J. Appl. Mech.
Kalanovic, V.D., Jenkins, C.H., and Haugen, F., “Fuzzy Control of Membrane Wrinkling,” Intell. Automation Soft. Comput.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Jenkins, C.H., Haugen, F. & Spicher, W.H. Experimental measurement of wrinkling in membranes undergoing planar deformation. Experimental Mechanics 38, 147–152 (1998). https://doi.org/10.1007/BF02321658
Received:
Revised:
Issue Date:
DOI: https://doi.org/10.1007/BF02321658