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NASA Scientific and Technical Aerospace Reports

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20040121019 <strong>NASA</strong> Langley Research Center, Hampton, VA, USA<br />

Taguchi Approach to Design Optimization for Quality <strong>and</strong> Cost: An Overview<br />

Unal, Resit; Dean, Edwin B.; [1990]; 10 pp.; In English; 1991 Annual Conference of the International Society of Parametric<br />

Analysts, 1 Jan. 1991, USA; No Copyright; Avail: CASI; A02, Hardcopy<br />

Calibrations to existing cost of doing business in space indicate that to establish human presence on the Moon <strong>and</strong> Mars<br />

with the Space Exploration Initiative (SEI) will require resources, felt by many, to be more than the national budget can afford.<br />

In order for SEI to succeed, we must actually design <strong>and</strong> build space systems at lower cost this time, even with tremendous<br />

increases in quality <strong>and</strong> performance requirements, such as extremely high reliability. This implies that both government <strong>and</strong><br />

industry must change the way they do business. Therefore, new philosophy <strong>and</strong> technology must be employed to design <strong>and</strong><br />

produce reliable, high quality space systems at low cost. In recognizing the need to reduce cost <strong>and</strong> improve quality <strong>and</strong><br />

productivity, Department of Defense (DoD) <strong>and</strong> National Aeronautics <strong>and</strong> Space Administration (<strong>NASA</strong>) have initiated Total<br />

Quality Management (TQM). TQM is a revolutionary management strategy in quality assurance <strong>and</strong> cost reduction. TQM<br />

requires complete management commitment, employee involvement, <strong>and</strong> use of statistical tools. The quality engineering<br />

methods of Dr. Taguchi, employing design of experiments (DOE), is one of the most important statistical tools of TQM for<br />

designing high quality systems at reduced cost. Taguchi methods provide an efficient <strong>and</strong> systematic way to optimize designs<br />

for performance, quality, <strong>and</strong> cost. Taguchi methods have been used successfully in Japan <strong>and</strong> the USA in designing reliable,<br />

high quality products at low cost in such areas as automobiles <strong>and</strong> consumer electronics. However, these methods are just<br />

beginning to see application in the aerospace industry. The purpose of this paper is to present an overview of the Taguchi<br />

methods for improving quality <strong>and</strong> reducing cost, describe the current state of applications <strong>and</strong> its role in identifying cost<br />

sensitive design parameters.<br />

Author<br />

Taguchi Methods; Quality Control; Total Quality Management; Design Analysis<br />

39<br />

STRUCTURAL MECHANICS<br />

Includes structural element design, analysis <strong>and</strong> testing; dynamic responses of structures; weight analysis; fatigue <strong>and</strong> other structural<br />

properties; <strong>and</strong> mechanical <strong>and</strong> thermal stresses in structures. For applications see 05 Aircraft Design, Testing <strong>and</strong> Performance; <strong>and</strong><br />

18 Spacecraft Design, Testing <strong>and</strong> Performance.<br />

20040111124 S<strong>and</strong>ia National Labs., Albuquerque, NM, USA<br />

Four-Parameter Iwan Model for Lap-Type Joints<br />

Segalman, D. J.; Nov. 2002; In English<br />

Report No.(s): DE2004-805877; SAND2002-3828; No Copyright; Avail: National <strong>Technical</strong> Information Service (NTIS)<br />

The constitutive behavior of mechanical joints is largely responsible for the energy dissipation <strong>and</strong> vibration damping in<br />

weapons systems. For reasons arising from the dramatically different length scales associated with those dis- sipative<br />

mechanisms <strong>and</strong> the length scales characteristic of the overall structure, this physics cannot be captured through direct<br />

numerical simulation(DNS) of the contact mechanics within a structural dynamics analysis. The difficulties of DNS manifest<br />

themselves either in terms of Courant times that are orders of magnitude smaller than that necessary for structural dynamics<br />

analysis or as intractable conditioning problems. The only practical method for accommodating the nonlinear nature of joint<br />

mechanisms within structural dynamic analysis is through constitutive models employing degrees of freedom natural to the<br />

scale of structural dynamics. In this way, development of constitutive models for joint response is a prerequisite for a<br />

predictive structural dynamics capability. A four-parameter model, built on a framework developed by Iwan, is used to<br />

reproduce the qualitative <strong>and</strong> quantitative properties of lap-type joints. In the development presented here, the parameters are<br />

deduced by matching experimental values of energy dissipation in harmonic loading <strong>and</strong> values of the force necessary to<br />

initiate macro-slip. (These experiments can be performed on real hardware or virtually via fine-resolution, nonlinear<br />

quasi-static finite elements.) The resulting constitutive model can then be used to predict the force/displacement results from<br />

arbitrary load histories.<br />

NTIS<br />

Energy Dissipation; Vibration Damping; Weapon Systems<br />

20040111192 Building <strong>and</strong> Construction Research TNO, Delft, Netherl<strong>and</strong>s<br />

SUS: Survivability after Underwater Shock: Implementation of Whipping Bending Moment <strong>and</strong> Hull Plate Dishing<br />

Bos, J.; March 2004; 25 pp.; In English<br />

Contract(s)/Grant(s): A02/KM/109; TNO Proj. 006.38108<br />

Report No.(s): TD-2004-0103; Rept-2004-CMC-R013; Copyright; Avail: Other Sources<br />

134

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