Third International Conference on Inverse Design Concepts and Optimization in Engineering Sciences (ICIDES-3)

618 Pages·30.3 MB·English

by  NON

PROCEEDINGS
THIRD INTERNATIONAL CONFERENCE ON INVERSE DESIGN
CONCEPTS AND OPTIMIZATION IN ENGINEERING SCIENCES
ICIDES-III
October 23-25, 1991
Washington, D.C.
Sponsored by:
NASA HEADQUARTERS NATIONAL SCIENCE FOUNDATION
Aeronautics Directorate Division of Electrical and Communications Systems
Aerodynamics Division Communications & Computational Systems Program
600 Independence Avenue, SW 1800 G Street, NW
Washington, D.C. 20546 Washington, D.C. 20550
OFFICE OF NAVAL RESEARCH PENN STATE UNIVERSITY
Department of the Navy College of Engineering
Mechanics Division Department of Aerospace Engineering
800 North Quincy Street 233 Hammond Building
Arlington, VA 222171 University Park, PA 16802
Organized and edited by:
George S. Dulikravich
N92-i392
(NASA-CP.-I d8125) TH IRT) INIF_RNATIONAL
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FOREWORD
The need for organizing the ICIDES sequence of conferences arose in my mind almost a
decade ago while noticing that there were no established forums for the exchange of conceptual
ideas in the general field of inverse, semi-inverse, and direct design and optimization in
engineering sciences. There were neither specialized technical journals nor textbooks available in
this highly interdisciplinary field that rapidly grew with the availability of faster and larger
computing machines. Consequently, there were no technical courses in engineering programs that
would cover these design methodologies. The situation is starting to change, though, as a response
to increased interest on the part of industry which feels the pressure from the competitive global
market. ICIDES was envisioned as an open forum for experts and users alike to present their
methodologies and discuss their concepts.
The ICIDES sequence has experienced a steady growth in attendance, the number of
publications, and the international character of its audience, while maintaining high standards.
Locations Dates Papers Countries Sponsors
ICIDES-I Univ. of Texas at Austin Oct. 17-18, 1984 31 9 UT-Austin
ICIDES-I! Penn State University Oct. 24-26. 1987 32 9 NSF,ONR,PSU
ICIDES-III Washington, D.C. Oct. 23-25. 1991 48 15 NSF,ONR.NASA,PSU
Each contributed technical paper was reviewed by two colleagues without revealing to them
the identities of the authors. Although unusual, this process has stimulated more substantial and
constructive comments from the reviewers and has contributed to the improvements in the quality
of the accepted technical papers. Invited lectures at ICIDES-III form a unique collection of survey
articles that present a status report on the present state of the art worldwide.
ICIDES-III would not have been possible without financial support from NASA
Headquarters (Ms. Pamela Richardson and Mr. Louis Williams), ONR-Mechanics Division (Dr.
Philip Abraham and Dr. Spiridon Lekoudis), and NSF-Communications and Computational
Systems Program (Dr. George Lea). I would also like to thank my student assistants, Mr. Branko
Kosovic and Mr. Scott Sheffer for their help with the word processing of the conference
announcements. Finally, I would like to thank the authors and reviewers of the technical papers
and to the invited lecturers who contributed to the success of the ICIDES-III.
University Park, PA George S. Dulikravich
September 1991
ii
PRECEDING PAGE n, ,,,,,,,,

TABLE OF CONTENTS
Page
Foreword
George S. Dulikravich ii
Review of Aerodynamic Design in the Netherlands (Invited)
T. E. Labruj_re, National Aerospace Lab. NLR, Anthony Fokkerweg 2, 1059
CM Amsterdam, THE NETHERLANDS
/
Aerodynamic Aircraft Design Methods and their Notable Applications
-- Survey of the Activity in Japan (Invited)
K. Fujii , Inst. of Space & Astro. Science, Yoshinodai 3-1-1, Sagamihara,
Kanagawa, 229, JAPAN
S. Takanashi, NAL, Jindaiji-Higashi 7-44-1, Chofu, Tokyo 182, JAPAN
31 ,
On a Global Aerodynamic Optimization of a Civil Transport Aircraft
G. Savu and O. Trifu, The Aviation Institute, Bd. Pacii 220, 77538 Bucharest,
ROMANIA
45 _
Inverse Airfoil Design Procedure Using a Multigrid Navier-Stokes
Method
J.B. Malone and R.C. Swanson, Mail Stop 173, NASA Langley Research
Center, Hampton, VA 23665-5225, USA 55.
i,
A Comparison of Two Closely-Related Approaches to Aerodynamic
Design Optimization
G. R. Shubin and P. D. Frank, Org. G-6412, M/S 7L-21, Boeing Computer
Services, P.O. Box 24346, Seattle, WA 98124-0346, USA 67
Design of Thrust Vectoring Exhaust Nozzles for Real-Time
Applications Using Neural Networks
K. Prasanth, R. E. Markin and K.W. Whitaker, The University of Alabama,
Dept. of Aerospace Engineering, Tuscaloosa, AL 35487-0280, USA 79
Finite Element Structural Redesign by Large Admissible
Perturbations
M.M. Bernitsas, E. Beyko, C.W. Rim and B. Alzahabi, Dept. of Naval
Architecture and Marine Engineering, The University of Michigan-North
Campus, Ann Arbor, MI 48109-2145, USA 87
Structural Damage Indentification Using Mathematical Optimization
Techniques
M.H.H. Shen, Ohio State University, Dept. of Aero. & Astro. Eng., 2036
Nell Avenue Mall, Columbus, OH 43210-1276, USA 99. :
Electrical Impedance Imaging in Two-Phase, Gas-Liquid Flows: to
Initial Investigation
J.T. Lin, L. Ovacik and O.C. Jones, Center for Multiphase Research, RPI,
Troy, N.Y. 12180-3590, USA
Recent Progress in Inverse Methods in France (Invited)
P. Bry ,SNECMA, Cincinnati, OH, USA and O. P. Jacquotte and M.-C. Le
Pape, Aerodynamics Dept.,ONERA, BP 72, 92322 Chatillon, FRANCE 123
°,°
Ul
Research on Inverse, Hybrid and Optimization Problems in
Engineering Sciences with Emphasis on Turbomachine
Aerodynamics: Review of Chinese Advances (Invited)
G.-L. Liu, Lab. for Turbomachinery Aerodynamics, Shanghai Institute of
Mech. Eng., 516 Jun-Gong Road, Shanghai 200093, P. R. CHINA 145
The Turbomachine Biading Design Using $2-S1 Approach
T.S. Luu, L. Bencherif and B. Viney, LIMSI (CNRS), BP 133, F-91403
Orsay Cedex, FRANCE, and
J. M. Nguyen Duc, SEP, BP 802, F-27207 Vernon, FRANCE 165
A Proposed Through-Flow Inverse Method for the Design of a
Mixed-Flow Pumps
J. E. B. T. Borges, Department of Mechanical Eng.,Instituto Superior Tecnico,
Av. Rovisco Pais, 1096 Lisboa, PORTUGAL 177 _
An Inverse Inviscid Method for the Design of Quasi-Three
Dimensional Rotating Turbomachinery Cascades
E. Bonataki, P. Chaviaropoulos and K.D. Papailiou, National Technical
University of Athens, Dept. of Mechanical Eng., Lab. of Thermal
Turbomachines, P.O. Box 64069, 15710 Athens, GREECE 189
A PC-Based Inverse Design Method for Radial and Mixed Flow
Turbomachinery
I. H. Skoe, IA-T, Kristion Sonjugvei 20, 3600 Kongsberg, NORWAY 201 :,_:
Optimal Design of Solidification Processes
J.A. Dantzig and D.A. Tortorelli, University of Illinois, Dept. of Mech. &
Indust. Eng., 140 Mechanical Eng. Bld., MC-244, 1206 West Green Street,
Urbana, Illinois 61801, USA 213
Numerical Identification of Boundary Conditions on Nonlinearly
Radiating Inverse Heat Conduction Problems
D. A. Murio, Dept. of Math. Sciences, Old Chemistry Bldg. (ML 25),
University of Cincinnati, Cincinnati, OH 45221-0025, USA 227
Comparison of Four Stable Numerical Methods for Abel's Integral
Equation
D. A. Murio and C. E. Mejia, Dept. of Math. Sciences, Old Chemistry Bldg.
(ML 25), University of Cincinnati, Cincinnati, OH 45221-0025, USA 239,
Optimization of the Heating Surface Shape in the Contact Melting
Problem
S.A. Fomin, Dept. of Appl. Math., Kazan State University, Kazan, 420008,
USSR
S.-M. Cheng, Dept .of Power Eng., Huazhong University of Science and
Technology, Wuhan 430074, P. R. CHINA 253 <
Design of 3-Dimensional Complex Airplane Configurations with
Specified Pressure Distribution via Optimization (Invited)
K. Kubrynski, Tech. Univ. of Warsaw, Institute of Applied Mechanics and
Aviation Technology, ul. Nowowiejska 24, 00-665 Warsaw, POLAND
iv
Extended Mapping and Characteristics Techniques for Inverse
Aerodynamic Design
H. Sobieczky, DLR-Inst. fuer Theoret. Stroemung., Bunsenstrasse 10, 3400
Goettingen, F. R. GERMANY
Y.-J. Qian, Beijing Univ. of Aero. & Astro., 37 Xue Yuan Road, Haidian
District, Beijing 100083, P. R. CHINA
Supercritical Blade Design on Stream Surfaces of Revolution with an
Inverse Method
E. Schmidt and H-D. Grein, Inst. fuer Aero. & Gas Dynamik, University of
Stuttgart, Pfaffenwaldring 21, D-7000 Stuttgart 80, F. R. GERMANY 293-
Applications of Direct Inverse Analogy Method (DIVA) and Viscous
Design Optimization Techniques
E. Greff, D. Forbrich and H. Schwarten, Deutsche Airbus GmbH, Dept. of
Aerodynamics, Postfach 107845, D-2800 Bremen 1, F. R. GERMANY 307 "
Blade Design and Analysis Using A Modified Euler Solver
O.Leonard and R.A. Van den Braembussche, yon Karman Institute, Chauss6e
de Waterloo 72, 1640 Rhode-Saint-Genese, BELGIUM 325= -
Variational Formulation of Hybrid Problems for Fully 3-D Transonic
Flow With Shocks in Rotor
G.-L. Liu, Lab. for Turbomachinery Aerodynamics, Shanghai Institute of
Mech. Eng., 516 Jun-Gong Road, Shanghai 200093, P. R. CHINA 337.
Aerodynamic Shape Optimization of Arbitrary Hypersonic Vehicles
G. S. Dulikravich and S. G. Sheffer, Dept. of Aerospace Eng.,
The Pennsylvania State University, University Park, PA 16802, USA 347 -
Analysis and Design of Transonic Airfoils Using Streamwise
Coordinates
R. M. Barton and C.-F. An, Dept. of Mathematics and Statistics, University of
Windsor, 401 Sunset, Windsor, Ontario N9B 3P4, CANADA 359
Research on Inverse Design Methods and Optimization in Italy
(Invited)
F. Larocca, FIAT AVIO, Corso Ferruci 112, 10129 Torino, ITALY 371 :-
Adjoint Operator Approach to Shape Design For Internal
Incompressible Flows (Invited)
H. Cabuk, C.-H. Sung and V. Modi, Mech. Eng. Dept., 220 Mudd Hall,
Columbia University, New York, NY, 10027, USA 391 r:: -:,
+'
An Inverse Method for the Aerodynamic Design of Three-
Dimensional Aircraft Engine Nacelles
R.A. Bell and R.D. Cedar, G.E. Aircraft Engines, One Neuman Way, MD
A317, Cincinnati, OH 45215-6301, USA
Vortex Generator Design for Aircraft Inlet Distortion as a Numerical
Optimization Problem
B.H. Anderson, NASA Lewis Research Center, Mail Stop 5-11, 21000
Brookpark Road, Cleveland, OH. 44135, USA
R. Levy, Scientific Research Associates, Inc., 50 Nye Road, P.O. Box 1058,
Glastonbury, CT 06033, USA
419.:. /
v
Airfoil Optimization With Efficient Gradient Calculations
T. Sorensen, MIT, Dept. of Aero. & Astro., 77 Massachusetts Ave, Room 37-
350, Cambridge, MA 02139, USA 433 " /
Design Optimization of Transonic Airfoils
C.-Y. Joh, B. Grossman and R.T. Haftka, VPI, Aero. & Ocean Eng.Dept.,
214 Randolph Hall, Blacksburg, VA 24061, USA
Identification of Dynamic Characteristics of Flexible Rotors as a
Dynamic Inverse Problem
W.P. Roisman and L.D. Vajingortin, Department of Applied Mechanics,
Khmelnitsky Technological Institute, 11 Institutskaja Ulica, Khmelnitsky,
280016, USSR 457 z-
On Designing for Quality
L.D. Vajingortin and W.P. Roisman, Department of Applied Mechanics,
Khmelnitsky Technological Institute, 11 Institutskaja Ulica, Khmelnitsky,
280016, USSR 469 )'_
Optimal Interaction of Indenter With Inhomogeneous Plate
V. N. Aptukov, Lab. of Impulse Deformation of Bodies, Inst. of Continuous
Media Mech., Acad. of Sci. of USSR, Koroleva Ulica 1, Perm, 614061,
USSR
Analysis of the Optimal Laminated Target Made up of Discrete Set of
Materials
V. N. Aptukov and V.L. Belousov, Laboratory of Impulse Deformation of
Bodies, Institute of Continuous Media Mechanics, Academy of Sciences of
USSR, Koroleva Ulica 1, Perm, 614061, USSR 489 'i
Inverse Problems in the Design, Modeling and Testing of
Engineering Systems (Invited)
O. M. Alifanov, College of Cosmonautics, Moscow Aviation Institute,
4,Volokolamskoe sh., Moscow, 125871, USSR 495 i' :"
Inverse Problems and Optimal Experiment Design in Unsteady Heat
Transfer Processes Identification (Invited)
E. A. Artyukhin, College of Cosmonautics, Moscow Aviation Institute, 4,
Volokolamskoe sh., Moscow, 125871, USSR 513 r
A New Method of Optimal Design for a Two-Dimensional Diffuser by
Using Dynamic Programming
C.-G. Gu, M.-J. Zhang, X. Chen and Y.-M. Miao, Department of Power
Machinery Eng., Xi'an Jiaotong University, Xi'an 710049, Shaanxi Province,
P. R. CHINA
Study of a New Airfoil Used in Reversible Axial Fans
C.-J. Li, B.-S Wei and C.-G. Gu, Department of Power Machinery Eng.,
Xi'an Jiaotong University, Xi'an, Shaanxi Province, P. R. CHINA 541
An Inverse Method With Regularity Condition for Transonic Airfoil
Design
Z.-Q. Zhu, Z.-X. Xia and L.-Y.Wu, Beijing University of Aeronautics and
Astronautics, 37 Xueyuan Road, Haidian District, Beijing 100083, P. R.
CHINA
553 ,.,_.
vi
Inverse Problems in Diffraction
A. G. Mikheev and A.S. Shamaev, Institute for Problems in Mechanics,
USSR Academy of Sciences, Pr. Vernadskogo 101, Moscow 117526,
USSR 563
Optimization of Transistor Design Including Large Signal
Device/Circuit Interaction at Extremely High Frequencies (20-100+
GHz)
R. Levy and H.L Grubin, Scientific Research Associates, Inc., 50 Nye Road,
P.O. Box 1058, Glastonbury, CT 06033, USA
573 U_
Design of Transonic Compressor Cascades Using Hodograph Method
Z.-Y. Chen and J.-R. Guo, Department of Thermal Engineering, Tsinghua
University, Beijing, P. R. CHINA 593
The Research Progress on Hodograph Method of Aerodynamic
Design at Tsinghua University
Z.-Y. Chen and J.-R. Guo, Department of Thermal Engineering, Tsinghua
University, Beijing, P. R. CHINA 599
The following papers have been accepted for presentation at the ICIDES-III, but their final
versions have not arrived in time to be included in the bound volume.
Numerical Optimization in Germany: A Non-Exhaustive Survey on
Current Developments with Emphasis on Aeronautics (Invited)
L. Fomasier, DASA-MBB GmbH, Ottobrunn, F.R. GERMANY
A Design Algorithm for 2D Cascade Flow
H. Ye and R. M. Barton, Dept. of Mathematics and Statistics, University of
Windsor, 401 Sunset, Windsor, Ontario N9B 3P4, CANADA
vii