Introduction Cum Need for a Scramjet Engine
History
Working
More information about Scramjet Engines
Hyper X Vehicle
Applications of scramjet engines
Challenges to scramjet engine technology
Conclusion
References
For further explanation:
https://www.youtube.com/watch?v=0Ux7mYSlAfg
about scramjets, its components, function, its advantages and advantages, its applications with many references by reshmi.r , dinesh kumar and sandeep.
A scramjet (supersonic combustion ramjet) engine is variant of a ramjet air breathing combustion jet engine in which the combustion process takes place in supersonic airflow.
A scramjet (supersonic combusting ramjet) is a variant of a ramjet air breathing jet engine in which combustion takes place in supersonic airflow. As in ramjets, a scramjet relies on high vehicle speed to forcefully compress the incoming air before combustion, but a ramjet decelerates the air to subsonic velocities before combustion, while airflow in a scramjet is supersonic throughout the entire engine. This allows the scramjet to operate efficiently at extremely high speeds
Scramjet Engine a variant of Ram jet engine.In this presentation you will find all necessary details about it.By this slide you have a broader idea about scramjet engine,its working,its uses,its scope in India.
India is also among those nations who have developed Scramjet engine.
about scramjets, its components, function, its advantages and advantages, its applications with many references by reshmi.r , dinesh kumar and sandeep.
A scramjet (supersonic combustion ramjet) engine is variant of a ramjet air breathing combustion jet engine in which the combustion process takes place in supersonic airflow.
A scramjet (supersonic combusting ramjet) is a variant of a ramjet air breathing jet engine in which combustion takes place in supersonic airflow. As in ramjets, a scramjet relies on high vehicle speed to forcefully compress the incoming air before combustion, but a ramjet decelerates the air to subsonic velocities before combustion, while airflow in a scramjet is supersonic throughout the entire engine. This allows the scramjet to operate efficiently at extremely high speeds
Scramjet Engine a variant of Ram jet engine.In this presentation you will find all necessary details about it.By this slide you have a broader idea about scramjet engine,its working,its uses,its scope in India.
India is also among those nations who have developed Scramjet engine.
AM PRESENTING U MA SEMINAR SLIDES ON TOPIC "HYPERSONIC AIR BREATHING ENGINES" ROOTED UP BY HELP OF NASA INFORMATION.SINCE I AM INTERESTED IN SPACE STUDIES I CHOOSE THIS,EVENTHOUGH AM A MECH ENGINEER!! ..I KNOW , SOMEONE OR ANYONE BE GAINFUL BY THIS.....DURING MA SEMINAR I HOLD ON MANY SITES TO PROVIDE RELATD SLIDES,BUT THEY ALL NEED REGISTRATION,MONEY AND ALL...BUT ITZ NOT FAIR.!!...SO AM SHARING U WITH THIS.....FOR ANY DOUBTS OR REPORTS,SUPPORTING JOURNELS ,CONTACT ME: sanoojsiddikh@gmail.com
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This is a presentation that contains detailed information about hypersonic vehicle or hyperplanes travelling at speeds upto 6 times the speed of sound. It also contains information about some hyperplanes like nasa x43, avatar hyperplane. This presentation also deals with the selection of suitable design for hyperplanes.
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AM PRESENTING U MA SEMINAR SLIDES ON TOPIC "HYPERSONIC AIR BREATHING ENGINES" ROOTED UP BY HELP OF NASA INFORMATION.SINCE I AM INTERESTED IN SPACE STUDIES I CHOOSE THIS,EVENTHOUGH AM A MECH ENGINEER!! ..I KNOW , SOMEONE OR ANYONE BE GAINFUL BY THIS.....DURING MA SEMINAR I HOLD ON MANY SITES TO PROVIDE RELATD SLIDES,BUT THEY ALL NEED REGISTRATION,MONEY AND ALL...BUT ITZ NOT FAIR.!!...SO AM SHARING U WITH THIS.....FOR ANY DOUBTS OR REPORTS,SUPPORTING JOURNELS ,CONTACT ME: sanoojsiddikh@gmail.com
This ppt will explain about the new mode of transportation, i.e., Hyperloop which was proposed by ELON MUSK. It will feature its design, concept, working model, need, advantages and disadvantages.
This is a presentation that contains detailed information about hypersonic vehicle or hyperplanes travelling at speeds upto 6 times the speed of sound. It also contains information about some hyperplanes like nasa x43, avatar hyperplane. This presentation also deals with the selection of suitable design for hyperplanes.
We are confident that Compressed Air Technology (CAT) holds the key to the automobile's future. At the same time, though we are aware that no one type of vehicle. Can meet all society’s needs. That's why we are pushing ahead with research on a range of Vehicle propulsion technologies.
This PPT provides a complete overview of jet engine.
It includes several topics related to jet engine.
The topics are introduction, need, working principle, brayton cycle, types, application, merits & demerits, conclusion and future scope.
Proulsion I - SOLVED QUESTION BANK - RAMJET ENGINESanjay Singh
The material is only for academic purpose and for preparation of exams. Contents are copied from reference books. Not for revenue generation of any kind.
In this slide, 8 parameters are being considered to define the wind turbine blade efficiency and finally I have concluded some of the best conditions to get the optimum efficiency.
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The design and development of a hovercraft prototype with full hovercraft basic functions is
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fabrication skill. In-depth research was carried out to determine the components of a hovercraft
system and their basic functions and in particular its principle of operation. Detailed research in design
was done to determine the size of component parts, quite in accordance with relevant standard
requirements as applicable in the air cushioned vehicles (ACV). The fabrication of the designed
hovercraft by using materials that are readily available by taking into consideration the economic
constraints and time constraints. It also includes the testing process which includes the tweaking of
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Final project report on grocery store management system..pdfKamal Acharya
In today’s fast-changing business environment, it’s extremely important to be able to respond to client needs in the most effective and timely manner. If your customers wish to see your business online and have instant access to your products or services.
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About
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
Technical Specifications
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
Key Features
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface
• Compatible with MAFI CCR system
• Copatiable with IDM8000 CCR
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
Application
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
CFD Simulation of By-pass Flow in a HRSG module by R&R Consult.pptxR&R Consult
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R&R and Tetra Engineering Group Inc. were asked to solve the issue with reduced steam production.
An inspection had shown that a significant amount of hot flue gas was bypassing the boiler tubes, where the heat was supposed to be transferred.
R&R Consult conducted a CFD analysis, which revealed that 6.3% of the flue gas was bypassing the boiler tubes without transferring heat. The analysis also showed that the flue gas was instead being directed along the sides of the boiler and between the modules that were supposed to capture the heat. This was the cause of the reduced performance.
Based on our results, Tetra Engineering installed covering plates to reduce the bypass flow. This improved the boiler's performance and increased electricity production.
It is always satisfying when we can help solve complex challenges like this. Do your systems also need a check-up or optimization? Give us a call!
Work done in cooperation with James Malloy and David Moelling from Tetra Engineering.
More examples of our work https://www.r-r-consult.dk/en/cases-en/
Hybrid optimization of pumped hydro system and solar- Engr. Abdul-Azeez.pdffxintegritypublishin
Advancements in technology unveil a myriad of electrical and electronic breakthroughs geared towards efficiently harnessing limited resources to meet human energy demands. The optimization of hybrid solar PV panels and pumped hydro energy supply systems plays a pivotal role in utilizing natural resources effectively. This initiative not only benefits humanity but also fosters environmental sustainability. The study investigated the design optimization of these hybrid systems, focusing on understanding solar radiation patterns, identifying geographical influences on solar radiation, formulating a mathematical model for system optimization, and determining the optimal configuration of PV panels and pumped hydro storage. Through a comparative analysis approach and eight weeks of data collection, the study addressed key research questions related to solar radiation patterns and optimal system design. The findings highlighted regions with heightened solar radiation levels, showcasing substantial potential for power generation and emphasizing the system's efficiency. Optimizing system design significantly boosted power generation, promoted renewable energy utilization, and enhanced energy storage capacity. The study underscored the benefits of optimizing hybrid solar PV panels and pumped hydro energy supply systems for sustainable energy usage. Optimizing the design of solar PV panels and pumped hydro energy supply systems as examined across diverse climatic conditions in a developing country, not only enhances power generation but also improves the integration of renewable energy sources and boosts energy storage capacities, particularly beneficial for less economically prosperous regions. Additionally, the study provides valuable insights for advancing energy research in economically viable areas. Recommendations included conducting site-specific assessments, utilizing advanced modeling tools, implementing regular maintenance protocols, and enhancing communication among system components.
2. Contents
• Introduction Cum Need for a Scramjet Engine
• History
• Working
• More information about Scramjet Engines
• Hyper X Vehicle
• Applications of scramjet engines
• Challenges to scramjet engine technology
• Conclusion
• References
3. Introduction cum Need for Scramjet
Engines
• Nearly 70% of the propellant (fuel-oxidiser
combination) carried by today’s launch vehicles
consists of oxidiser.
• Launch vehicles (Rockets) designed for one time use
are expensive and their efficiency is low because they
can carry only 2-4% of their lift-off mass to orbit.
• That's the idea behind a different propulsion system
called "scramjet“.
• The oxygen needed by the engine to combust is taken
from the atmosphere passing through the vehicle,
instead of from a tank onboard. The craft becomes
smaller, lighter and faster.
• How fast? Researchers predict scramjet speeds could
reach 15 times the speed of sound. An 18-hour trip to
Tokyo from New York City becomes a 2-hour flight.
4. History
• In the 1950s and 1960s a variety of experimental
scramjet engines were built and ground tested in
the US and the UK.
• However, the first successful scramjet engine
flight test was done in 2002 by Australia. And
until today there are only 4 countries that have
demonstrated scramjet engine technology.
(Why did it take more than 40 years to realize this
technology?)
5. Working Principle
• For understanding the principle of scramjets,
we first need to understand the principle of
turbojets.
6. A turbojet engine is a gas turbine engine that works by
1) compressing air with an inlet and a compressor,
2) mixing fuel with the compressed air, burning the mixture in the combustor,
3) and then passing the hot, high pressure air through a turbine and a nozzle.
Note: Here, turbine is only used to run the compressor.
7. • Now, let’s move from turbojet engine to
ramjet engine.
• Ramjet engines have no moving parts unlike
turbojets or turbofans. It is an open duct
constituted of an inlet, a combustion chamber
and a nozzle.
8. If it doesn’t have a compressor then how is the air compressed before
the fuel ignition?
By Ram Effect
At flight numbers greater than 2, the incoming air, if captured and
decelerated properly, can be compressed to required pressure.
And hence if we do not need a compressor then we do not need a
turbine.Therfore, we do not have any moving part inside a Ramjet
Engine.
However, a ramjet engine only functions if it is moving at mach
number of greater than 2.Therefore it cannot take off and land by
itself.
(introduction of SR-71 blackbird)
9. Scramjet Engines
• At flight speeds of more than Mach 5, the
efficiency of a ramjet engine decreases.
Therefore, we use scramjet engines over Mach 5.
• Remember the only difference between a ramjet
engine and the scramjet engine is that the
combustion in ramjet engine is done subsonically.
But in scramjet engines, there is supersonic
combustion. Hence called “scramjet” or
supersonic ramjet.
11. More information about Scramjet
Engines
• In scramjet engines, the engine is airframe
integrated as shown in figure below.
• Also, since the flow is supersonic, the flow
is accompanied with shocks.
13. Applications of scramjet engines
1)Space applications
• An alternative to rockets
• Rockets carry their own liquid oxygen with
them(for combustion)and therefore the payload
they can carry is only 2-4% of their lift-off mass.
• However, scramjets use atmospheric oxygen for
combustion which helps them to carry more
payload.
• Therefore, Scramjets can help reduce the cost of
satellite launching business to very large extent.
14. 2) Military applications
• Used in missiles
• Scramjet missiles are better than ballistic
missiles because of better maneuverability
and higher speed.
15. 3) Civil Applications
• Researchers predict scramjet speeds could
reach 15 times the speed of sound.
• An 18-hour trip to Tokyo from New York City
becomes a 2-hour flight.
16. Challenges to scramjet Engines
• It’s time to answer the question we put earlier.
• Why did it take more than 40 years to realize
scramjet engine technology?
• Scramjet engines are simple in the sense that it
doesn’t have any moving parts but applying
scramjet technology into reality is not that
simple.
We will address some of these challenges in this
section.
17. 1) Residence Time
Flow speed are very large in the combustion
chamber(Mach 2.2). Therefore the residence
time, the time for fuel-air mixing and
combustion in a combustion chamber of a
particular length becomes very
small(milliseconds).
18. 2) Engine-Airframe integration
• Boeing makes the airframe and Pratt& Whitney
makes the engine .So, the expertise of airframe
making and engine making are not in the same
place.(and that’s okay for a commercial aircraft)
• But you can’t do this separately for a scramjet
engine. The engine in a scramjet vehicle is a part
of the airframe. It is because there is a big
aerodynamic coupling between the two
things.And therefore, testing of scramjet engines
need the two areas to merge together.
19. 3) Drag
If you want a reasonable residence time, the
length of the vehicle has to be large. But if you
do that, the drag on the vehicle increases. As
the drag is not only on the airframe but also
on the inside of the engine. And the engine
length is comparable to vehicle length.
20. 4)Testing
• Building a wind tunnel for the scramjet
engines is very expensive.
• It is because to test any engine for supersonic
speeds the power required for testing even for
a very small time is very large.
21. 5) Scalability
• Now that testing is expensive. We go for small
scale testing. But the scalability becomes
another problem.
• Scalability is difficult for a circular intake. But,
it is good for a rectangular intake.
22. Conclusion
• Today, satellites are launched into orbit by multi-staged
satellite launch vehicles that can be used only once
(expendable)
• If those vehicles are made re-usable by scramjet engine
technology, the cost of launching satellites will further
come down significantly. Thus, the future re-usable
launch vehicle concept along with air-breathing
propulsion is an exciting candidate offering routine
access to space at far lower cost.
• There are a lot of challenges to the scramjet engine
technology. But it’s tonnes of applications make it
worth of more research.
23. REFERENCES
• ISRO’s Scramjet Engine Technology Demonstrator Successfully Flight Tested
https://www.isro.gov.in/launchers/isro%E2%80%99s-scramjet-engine-technology-demonstrator-successfully-
flight-tested
• What's a Scramjet?
https://www.nasa.gov/missions/research/f_scramjets.html
• Website: Scramjet
https://en.wikipedia.org/wiki/Scramjet
• X-51 Waverider Unmaned Scramjet Aircraft
https://www.airforce-technology.com/projects/x51-wave-rider/
• History of scramjet propulsion development
https://www.researchgate.net/publication/324946953_History_of_scramjet_propulsion_development
• Hyshot program secure place in flight history
https://www.uq.edu.au/news/article/2002/08/hyshot-program-secures-place-flight-history
• Corin Segal, The Scramjet Engine processes and characteristics, Cambridge publication press, 2009, ISBN-
13 978-0-511-65110-6