Supersonic intakes - aircraft engine, Other Engineering

Assignment Help:

SUPERSONIC INTAKES

At supersonic speeds, the pitot type of air intake is unsuitable due to the severity of shock waves which form and progressively reduce the intake efficiency as speed increases. To overcome this problem the compression intake was designed.

641_suspantion intake.png

 

This type of intake produces a series of mild shock waves without reducing the intake efficiency, as the aircraft speed increases, so also does the intake compression ratio. At high mach numbers it becomes necessary to have an air intake which has a variable thrust area and spill doors to control the column of air.

 


Related Discussions:- Supersonic intakes - aircraft engine

Inversion circle, what do you understand by inversion circle?

what do you understand by inversion circle?

Ewing’s molecular theory of magnetism, Ewing’s molecular theory of magnetis...

Ewing’s molecular theory of magnetism   Every molecule of a magnetic substance behaves as a tiny magnet called molecular magnet. In an unmagnetized state the molecular m

Chemical engineering project, Hello, I have a chemical engineering project...

Hello, I have a chemical engineering project and I need help.

Hardness of water, why is only 1 lime and sod required for aluminium impuri...

why is only 1 lime and sod required for aluminium impurities

Fire evacuation - railway inspections, Fire evacuation - Railway inspection...

Fire evacuation - Railway inspections: Fire evacuation signals should be given by voice messages and these must be easily understood by the occupants. The expected populati

Fiancial managment, Suppose you borrow $10,000 at 10% and you are going to ...

Suppose you borrow $10,000 at 10% and you are going to make monthly payments of $2,500. How long until you pay off the loan?

Problem Set, 1) An investment project requires a net investment of $100,000...

1) An investment project requires a net investment of $100,000. The project is expected to generate annual net cash flows of $28,000 for the next 5 years. The firm''''''''s cost of

Aerofoil aerodynamics -framework, Framework In the laboratory we will de...

Framework In the laboratory we will deal with low speed flows, at first using the potential flow solver. We will also investigate behaviour for the NACA 4-series of aerofoils.

Water supply design, what is the use of HEC-HMS modelling in water supply s...

what is the use of HEC-HMS modelling in water supply system ,how we use it? what is the necessary input for the software?

Write Your Message!

Captcha
Free Assignment Quote

Assured A++ Grade

Get guaranteed satisfaction & time on delivery in every assignment order you paid with us! We ensure premium quality solution document along with free turntin report!

All rights reserved! Copyrights ©2019-2020 ExpertsMind IT Educational Pvt Ltd