Library Subscription: Guest
ICHMT DL Home Current Year Archives Executive Committee International Centre for Heat and Mass Transfer

INVERSE DESIGN OF ENGINEERING SYSTEMS DOMINATED BY RADIATIVE TRANSFER

DOI: 10.1615/ICHMT.1997.IntSymLiqTwoPhaseFlowTranspPhenCHTRadTransfProc.200
19 pages

Francis Franka
Department of Mechanical Engineering The University of Texas at Austin, Austin, Texas, USA

Juan Carlos Morales
Department of Mechanical Engineering, The University of Texas at Austin, Austin, Texas, USA

Masahito Oguma
Research Laboratory, Ishikawajima Harima Heavy Industry Shin'nakahara 1, Isogo-ku, Yokohama, 235 JAPAN; Hokkaido University, Japan

John R. Howell
Department of Mechanical Engineering, The University of Texas at Austin, Austin TX 78712, U.S.A.

Abstract

Inverse radiative design techniques can eliminate much of the trial and error used in conventional or “forward” thermal design. Accurate determination of initial design parameters by inverse analysis can provide the necessary starting point for a detailed design using conventional detailed programs. If successful, this will free designers to determine with more accuracy the best design that will meet their requirements, and will not require limitation to iterative solutions and to the few cases that can normally be examined using conventional techniques. Here, we discuss some of the mathematical techniques for inverse design (Monte Carlo, singular value decomposition (SVD), modified truncated singular value decomposition (MTSVD), and conjugate gradient), their relative strengths and weaknesses, show results generated by some of these techniques for some example problems, and we also indicate some remaining challenges and opportunities for inverse design.

ICHMT Digital Library

Bow shocks on a jet-like solid body shape. Thermal Sciences 2004, 2004. Pulsed, supersonic fuel jets - their characteristics and potential for improved diesel engine injection. PULSED, SUPERSONIC FUEL JETS - THEIR CHARACTERISTICS AND POTENTIAL FOR IMPROVED DIESEL ENGINE INJECTION
View of engine compartment components (left). Plots of temperature distributions in centreplane, forward of engine (right). CHT-04 - Advances in Computational Heat Transfer III, 2004. Devel... DEVELOPMENT AND CURRENT STATUS OF INDUSTRIAL THERMOFLUIDS CFD ANALYSIS
Pratt & Whitney's F-135 Joint Strike Fighter Engine under test in Florida is a 3600F class jet engine. TURBINE-09, 2009. Turbine airfoil leading edge stagnation aerodynamics and heat transfe... TURBINE AIRFOIL LEADING EDGE STAGNATION AERODYNAMICS AND HEAT TRANSFER - A REVIEW
Refractive index reconstructed field. (a) Second iteration. (b) Fourth iteration. Radiative Transfer - VI, 2010. Theoretical development for refractive index reconstruction from a radiative ... THEORETICAL DEVELOPMENT FOR REFRACTIVE INDEX RECONSTRUCTION FROM A RADIATIVE TRANSFER EQUATION-BASED ALGORITHM
Two inclusion test, four collimated sources. Radiative Transfer - VI, 2010. New developments in frequency domain optical tomography. Part II. Application with a L-BFGS associated to an inexa... NEW DEVELOPMENTS IN FREQUENCY DOMAIN OPTICAL TOMOGRAPHY. PART II. APPLICATION WITH A L-BFGS ASSOCIATED TO AN INEXACT LINE SEARCH