1Engineering Laboratories, Northrop Corp., Norair Division, Hawthorne, California
This paper describes the work accomplished under contract AF 33 (616)-8429 (Task Study No. 5) "Feasibility cf Determining the Transfer Function for Selected Support Restraint Materials." A brief discussion of the mathematical model, describing the webbing material, is presented. Verification of the model by test and the limitations imposed by model representation are also described.
This presentation describes only the first step in resolving whether or not there exists a practical method of dynamic analysis of restraint materials.