Title: Aerospace%20Education%20
1Aerospace Education Research in the Area of
Design Diamond Jubilee Lectures
2003-04Department of Aerospace
EngineeringIndian Institute of Science, Bangalore
- K. Sudhakar
- Centre for Aerospace Systems Design Engineering
- Indian Institute of Technology
- Mumbai 400 076
- October 30, 2003
2Year 1997
- Technology Perspective The Next Decade
- Aeronautics Research Development Board
- ARDB/TC/001, May 1997
- Suggested centres of excellence to be
- supported by ARDB are
- CFD
- Advanced Composites
- Systems Design Engineering ? ?
3Years 1990 -1997
- Aerospace Design as a discipline at IITB
- Specialization dropped
- Courses had tapered off
- Design, Build Or Open ended problems shunned
- No research interest among faculty
?
- March 1998 ARDB Sanction arrives
4CASDE July 1998
- Mission
- CASDE shall strive to develop and retain strong
links with - Indian Aerospace Industry and shall engage in
RD activities with worldwide visibility
http//www.casde.iitb.ac.in/
5Objectives of CASDE
- M. Tech Programme in Systems Design Engineering
- Modeling Simulation Laboratory
- System Design Methodologies
- Awareness Creation
6M. Tech in Systems Design Engineering
- What do others teach?
- What can draw / retain student interest?
- What will faculty want to teach?
- What will industry want?
- What all should be taught?
- Form a composite team
- Brain-storming session
http//www.casde.iitb.ac.in/History/PastEvents/lon
avla/odw-see.pdf
7M. Tech in Systems Design Engineering
- Courses of study
- System Modeling Simulation
- Optimization for Engineering Design
- Systems Engineering Principles
- Statistical Methods for Analysis Design
- Multi-disciplinary Design Optimization (MDO)
- Applied Mechatronics (hands on course)
- System Level Studies RC Model Aircraft
- Also available as short courses
- Coordinates a Special Interest Group on MDO
(SIG-MDO)
http//www.casde.iitb.ac.in/edu/batch_2003/curricu
lum.htm
8Laboratory and Other Infrastructure
- Wind tunnel balance
- Propulsion system test facilities
- IMS Laboratory ? http//www.casde.iitb.ac.in/IM
SL/ - COTS sensors, actuators, . . . .
- R/C Model construction facilities, training
- Data acquisition cards
- Software
9IMS Laboratory
http//www.casde.iitb.ac.in/IMSL/resources.html
10Launch Vehicle Simulator from VSSC
http//www.casde.iitb.ac.in/IMSL/vssc.html
11Applied Mechatronics
- Hands on course
- 2 hrs lecture 3 hrs lab per week
- 2 projects
http//www.casde.iitb.ac.in/Mechatronics/
12Student Projects
Appreciated
http//www.casde.iitb.ac.in/IMSL/student-projects.
html
13ME Dual Degree Project HILS
- Flight Dynamics sensor models
- RTLinux Comedi
- Real time simulation
- Choose WP NGC
- On-board Computer?
- Use hobby grade actuators
- Out of window display
http//www.casde.iitb.ac.in/Publications/pdfdoc/vi
shisht-DDP-2003.pdf
14Flapping Wing Flight
- Dual-Degree Project in Aero Flapping wing
- Unsteady aerodynamics for prescribed motion
- Aero elastic analysis for prescribed actuation
- Wing construction - Polyurethane foam. (IDC)
- Actuation mechanism for testing. (Robotics)
- B. Tech Project in Robotics
- (Robotics group)
- Mechanism design
- Kinematics prescribed
- Loads prescribed
15Awareness Creation - 2003
- January - CEP in Applied Mechatronics
- February - 3rd Meeting of SIG-MDO
- April - Workshop on MDO _at_DRDL
- August - Brainstorming on System Analysis
- September - Int. Conf. MSO-DMES
16We also!
- Traveling Course on Design, Build and Fly.
(CASDEADA) Student Projects as Case Studies. - http//www.casde.iitb.ac.in/IMSL/des-bld-fly.ht
ml - Naval Institute of Aeronautical Technology,
Cochin. - Dept. of Aerospace Engineering, MIT, Chennai
- Dept. of Aerospace Engineering, Parks College of
Eng.,Coimbatore - AeSI Wright Flyer Design Competition. (CASDEADA)
- http//www.casde.iitb.ac.in/we-also/des-comp/
17We also!
- AeSI Schools Outreach Programme. (CASDEADA)
- 30 events, 103 Schools, 5,600 students
- (Good part of events by CASDE)
- http//www.casde.iitb.ac.in/we-also/school-out
reach/
18http//www.casde.iitb.ac.in/MDO/
19Systems Engineering Process
Context
Super System
Requirements to lower level
System
Solution from lower level
Sub System
- Level 1 Good understanding of system
knowledge base, heuristic - Computationally less
expensive - Usually not available for
new systems. - Level 3 Physics based modeling
computationally intensive, - applicable to new systems
(VV?)
20CASDE Activities
- Research activity
- High fidelity models in design loop ( CFD, . .)
- Multi-Disciplinary Analysis (MDA) leading to
- Multi-disciplinary Design Optimization (MDO)
21Challenges!
- Human / Admin
- People coming together (Design, A/D, Str, Prop,
Controls) - Synchronizing funds (taken care of by ARDB)
- Technical
- Non-availability of disciplinary codes
- Neither here nor there!
22MDO Elements
- Architectures
- Sensitivity Analysis
- Surrogate Modeling
- Variable Complexity
23MDO Elements
- Architectures
- Sensitivity Analysis
- Surrogate Modeling
- Variable Complexity
24MDO Elements
- Architectures
- Sensitivity Analysis
- Surrogate Modeling
- Variable Complexity
25User Supplied Gradients
26User Symbolic Maths
27Automatic Extraction of Formulae
28Gradients by ADIFOR
29ADIFOR Ver 2.0
- First applied to VLM
- Recently to 3-D Euler
- Multiblock, Structured grid
- Central difference, FVM
- JST scheme of artificial dissipation.
- Multistage Runge-Kutta schemes.
- Implicit residual smoothing and local time
stepping
Original Code ADIFORed Code
No of lines 4,090 11,889
Exec. time (min) 6.58 28.25
30ADIFOR Ver 2.0
? Error in Finite Difference Estimate of d(L/D)/d? Error in Finite Difference Estimate of d(L/D)/d? Error in Finite Difference Estimate of d(L/D)/d? Error in Finite Difference Estimate of d(L/D)/d?
? ??0.2 ??0.02 ??0.002 ??0.0002
3.06 38.10 4.44 7.08 77.25
4.11 2.46 1.73 1.56 15.09
31MDO Elements
- Architectures
- Sensitivity Analysis
- Surrogate Modeling
- Variable Complexity
32MDO Elements
- Architectures
- Sensitivity Analysis
- Surrogate Modeling
- Variable Complexity
33Design / MDO Studies
- WingOpt
- 3D Duct
- Hypersonic Vehicle
- Design under uncertainty
34MDO of Transport Aircraft Wing
353-D Duct Design
363D-Duct Design Using High Fidelity Analysis
- Low Fidelity Design Criteria
- Wall angle lt 6
- Diffusion angle lt 3
- 6 REQ lt ROC
- Fluent for CFD
- RSM / DOE
- DACE
37Parameterization of HSTDV Body
Design variables XD ?1, ?2, ?3 , ?n_plan , ?wc
, wfac_pl, tfac_pl,, Hcruise
38 Hypersonic Vehicle Discipline
Interactions
Analysis Model
Output
Input variable
Ext. Compression Model AM1
?1
Y1 l1, l2, l3, h1, h2, h3 Y2 ma , MI, ?, pst
Y1
?2
Ext. Configuration Model AM2
Y3 (X,Y,Z) Y4 TOGW , C.G., Vol, Fuel mass
?3
Aero Model AM3
Y5 CN, Cm, CA
?n_pl
Trim Model AM4
Y6 TOGW_up, ?T , ?T , D
?w_c
SW
Thrust Model AM5
Y7 Th_deliv, Lp, Mp
ST
Hcr
Performance Model AM6
Y8 Cruise Range
?n_pl, SW ?1, Hcr
Variables not shared
Y1 Response from AM1 required as
input in AM2
Shared variables
39MDO-Framework
40http//www.casde.iitb.ac.in/MDO/
41Publications
2000 2001 2002 2003
Journal 0 1 32 11
International Conferences 0 1 6 5
Core faculty 4
42Thank You
43Analysis for Design
44MDO-Architectures
45MDO-Architectures
Analysis ?
Y12
? Evaluator
46MDO-Architectures
z, y12, y21
473D-Duct Design Using High Fidelity Analysis
- Low Fidelity Design Criteria
- Wall angle lt 6
- Diffusion angle lt 3
- 6 REQ lt ROC
- Fluent for CFD
- RSM / DOE
- DACE
483D-Duct Design Using High Fidelity Analysis
- Low Fidelity Design Criteria
- Wall angle lt 6
- Diffusion angle lt 3
- 6 REQ lt ROC
- Fluent for CFD
- RSM / DOE
- DACE
http//www.casde.iitb.ac.in/MDO/3d-duct/
49MDA - System Analysis
50Design Analysis of Computer Experiments
- Regression fit Stochastic process
- Single global fit
- Variability in prediction known and exploitable
51Building Models Using DACE
5 predictive error
Use multi-modal GA to identify n highest
peaks. Test if they are higher than 5 Add
computer experiments at those spots
52Design - Publications
- Journal of Aircraft
- Volume 40 Number 4
- July 2003
- Total number of papers - 22
- Number of papers addressing design - 4