WELCOME TO THE AEROSPACE SCIENCE AND TECHNOLOGY … · • F-5 Aeroelasticity Project ... 1 - Basic...
Transcript of WELCOME TO THE AEROSPACE SCIENCE AND TECHNOLOGY … · • F-5 Aeroelasticity Project ... 1 - Basic...
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WELCOME TO THEWELCOME TO THE
AEROSPACE SCIENCE ANDAEROSPACE SCIENCE AND
TECHNOLOGY DEPARTMENTTECHNOLOGY DEPARTMENT
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� History
� Mission
� Organizational Structure
AGENDAAGENDA
� Organizational Structure
� Aeroelasticity in DCTA
� Final Remarks
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� History
� Mission
� Organizational Structure
AGENDAAGENDA
� Organizational Structure
� Aeroelasticity in DCTA
� Final Remarks
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August 8th, 1709
Lisbon, Portugal
The first public The first public presentation of a lighter-than-air aircraft model
Brazilian Dominican Priest Bartolomeu
Lourenço de Gusmão
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October 19th, 1901
Paris, France
The first certified flight of a The first certified flight of a dirigible aircraft
Brazilian self-made aeronautical engineer
Alberto Santos-Dumont
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November 12th, 1906
Paris, France
The first certified flight of an airplane
Alberto Santos-Dumont
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October 17th, 1935
Rio de Janeiro, Brazil
The first flight of a Brazilian designed airplane making serial production in Brazilian industry
Captain Antonio Guedes Muniz
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CTA Historical Evolution
1990198219711950
ITATechnological
Institute of Aeronautics
2006
Fli
gh
t Tests
Sp
ecia
l G
rou
p
19691954
IPDInstitute for
IAEAeronautical and Space
Institute
+IEAv
Institute for Advanced
Studies
IFIIndustrial
Fostering and Coordination
Institute
GEEVDCTA
Fli
gh
t Tests
Sp
ecia
l G
rou
p
IAESpace
Activities Institute
CTA
Institute for Research and Development
CTA1946
COCTA
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CTA First Project
Project Leader
Prof Henrich Focke
1940 1960
1951
1950 1970
CONVERTIPLANO
Heliconair-HC-1
1951 - 1956
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IPD Beija-Flor BF-01
1956 - 1965
CTA Second Project
1950
1956
Project Leader
Prof Henrich Focke
1960 1980
First Flight – DEC 1958
1970
1960
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Project Leader
Prof Max Holste
CTA Third Project
Oct 26th, 1968
1950 1970
Twin-engine Bandeirante
1965
1960 1980
1968
1st
flig
ht
Sta
rt
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1940 1960
1969: EMBRAER
1969
1950 1970
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� History
� Mission
� Organizational Structure
AGENDAAGENDA
� Organizational Structure
� Aeroelasticity in DCTA
� Final Remarks
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NATIONAL POWER
NationalNational Power Power DoctrineDoctrine
Political PowerPolitical Power
Economic Power
Psychossocial Power
S&T Power
Military Power
MILITARY POWERMILITARY POWER
Maritime Power
Land Power
Aerospace PowerAEROSPACE POWER
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1. Civil Aviation
2. Military Aviation
3. Airport Infra-structure
Aerospace Power
3. Airport Infra-structure
4. Aerospace Industry
5. Scientific and Technological Complex
6. Specialized Human Resources
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COMAER
EMAER SEFAHigh Staff Finances
ARMY NAVY
MINISTRY OF DEFENSE
Army NavyAir Force
COMGAR COMGAP COMGEP DCTA DEPENS DECEA
Air Operations Logistics HR S&T Education Airspace Control
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Brazilian Air Force
Combat Aircraft Replacement• Development of a national air fighter
NationalNational StrategyStrategy ofof DefenseDefenseNationalNational StrategyStrategy ofof DefenseDefense
Strategical Objectives
Focus on the Amazon region• Unities with technical resources to assure the operation of the landing runways and of the flight protection aids in order to maintain the proper conditions for survillance and combat
São José dos Campos S&T Complex• To prepare civil and military human resources• To develop dual application technologies• To strength ties with industry
• Development of a national air fighter
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MISSIONMISSION
To increase the knowledge and to develop
technological solutions to strengthen the
Aerospace Power, by means of education,
research, development, innovation, and
specialized services in aerospace technology,
contributing to the National Sovereignty and
to Brazilian society progress.to Brazilian society progress.
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� History
� Mission
� Organizational Structure
AGENDAAGENDA
� Organizational Structure
� Aeroelasticity in DCTA
� Final Remarks
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VDCTA
SDF SDA SDDPSDT
ADVISORY COUNCIL
DCTA
IFIIEAvIAEITA GIA
EDUCATION
AND
RESEARCH
INDUSTRIAL
LINK
INFRASTRUCTURE
AND SUPPORT
CLA CLBI
RESEARCH AND
DEVELOPMENT
GEEV TEST UNITS
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AeronauticsEducation &Research
Air Weapons
Space
Projects & Activities
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TECHNOLOGICAL INSTITUTE OF AERONAUTICSTECHNOLOGICAL INSTITUTE OF AERONAUTICS
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Engineering Levels
5 - Conception
4 - Development
3 - Production
2 - Maintenance
1 - Operation Air Marshall Eng Casimiro
Montenegro Filho
ITA/CTA Founder
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ITA Engineering Degrees
� Aerodynamics� Applied
Electronics �� Scientific
AeronauticalAeronautical / /
AerospaceAerospace
EngineeringEngineering
ElectronicalElectronical
EngineeringEngineering
MechanicalMechanical
EngineeringEngineeringCivil Civil
EngineeringEngineering
ComputerComputer
EngineeringEngineering
Aerodynamics
� Structures
� Propulsion
� Flight Mechanics
� Design
Electronics
� Circuits and Microwaves
� Control Systems
� Telecomuni-cations
� Energy
� Design
� Organization
� Technology
�� ScientificComputing
�Software Engineering
� Computing Theory
� Buildings
� Geotechnics
� Hydraulics
� Transports
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� Aerodynamics,
AeronauticalAeronautical andand
MechanicalMechanical
EngineeringEngineering
� Transportation
Infrastructure
ElectronicalElectronical andand
ComputerComputer
EngineeringEngineering
Civil Civil
AeronauticalAeronautical
EngineeringEngineeringPhysicsPhysics
� Electronic Systems
and Devices
� Atomic and
Molecular Physics
ITA Graduate Courses
� Aerodynamics,
Propulsion, and Energy
� Solid Mechanics and
Structures
� Physics and
Chemistry of
Aerospace Materials
� Industrial Production
� Aerospace Systems
and Mechatronics
�Professional Master
Degrees with Industry
Infrastructure
� Air Transportation
and Airports
and Devices
� Information
Technology
� Microwaves and
Optoelectronics
� Systems and
Control
� Telecomunications
Molecular Physics
� Nuclear Physics
� Plasma Physics
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FlightFlight TestTest CoursesCourses
Flight Test Special Group
One Class per YearOne Class per Year
– Duration: 45 weeks
Two Simultaneous Curricula
– Fixed Wing
– Rotary-Wing
Typical Class Composition
– 6 Test Pilots (4 fixed, 2 rotary-wing)
– 6 Flight Test Engineers
(4 fixed, 2 rotary-wing)
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Defense Systems
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Space Systems
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Laboratories
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� History
� Mission
� Organizational Structure
AGENDAAGENDA
� Organizational Structure
� Aeroelasticity in DCTA
� Final Remarks
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• The beginning – Prof Theodorsen (1950’s)
• undergraduate course
• The middle ages – Prof Bismarck (1970’s)
• graduate courses
Aeroelasticity in DCTA
• graduate courses
• The maturity – Research (1990’s)
• F-5 Aeroelasticity Project
• Brazilian Satellite Launch Vehicle (VLS)
• A last tribute
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General Theory of
Aerodynamic Instability
and the Mechanism of
Flutter – NACA Report
No. 496, 1935
Theodorsen’s Problem
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• The beginning – Prof Theodorsen (1950’s)
• undergraduate course
• The middle ages – Prof Bismarck (1970’s)
• graduate courses
Aeroelasticity in DCTA
• graduate courses
• The maturity – Research (1990’s)
• F-5 Aeroelasticity Project
• Brazilian Satellite Launch Vehicle (VLS)
• A last tribute
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PROF DR MAHER NASR
BISMARCK-NASR
1940 - 2008
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• The beginning – Prof Theodorsen (1950’s)
• undergraduate course
• The middle ages – Prof Bismarck (1970’s)
• graduate courses
Aeroelasticity in DCTA
• graduate courses
• The maturity – Research (1990’s)
• F-5 Aeroelasticity Project
• Brazilian Satellite Launch Vehicle (VLS)
• A last tribute
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MAA-1 Missile Integration
Flight Tests
Aeroelasticity of the F-5
Flight Tests
Subsonic and Supersonic
Aeroelastic Models
Ground
Vibration
Tests (GVT)
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Satellite Launch Vehicle (VLS-1)
Institute of Aeronautics and Space
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• The beginning – Prof Theodorsen (1950’s)
• undergraduate course
• The middle ages – Prof Bismarck (1970’s)
• graduate courses
Aeroelasticity in DCTA
• graduate courses
• The maturity – Research (1990’s)
• F-5 Aeroelasticity Project
• Brazilian Satellite Launch Vehicle (VLS)
• A last tribute
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PROF DR HOLT ASHLEY
1923 - 2006
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� History
� Mission
� Organizational Structure
AGENDAAGENDA
� Organizational Structure
� Aeroelasticity in DCTA
� Final Remarks
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TECHNOLOGY READINESS LEVELS
9 - Actual system “flight proven” through successful mission operations
8 - Actual system completed and “flight qualified” through test and
demonstration
7 - System prototype demonstration in an operational environment
6 - System/subsystem model or prototype demonstration in a relevant
environment
INNOVATION
environment
5 - Component and/or breadboard validation in relevant environment
4 - Component and/or breadboard validation in laboratory environment
3 - Analytical and experimental critical function and/or characteristic
proof of concept
2 - Technology concept and/or application formulated
1 - Basic principles observed and reported
SCIENCE
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311
248200
250
HUMAN RESOURCES
50
100
150 PhD
MSc
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To develop the power of our wings!To develop the power of our wings!To develop the power of our wings!To develop the power of our wings!