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

Assignment, Financial Management, Finance This case has been framed in orde...

Financial Management, Finance This case has been framed in order to test the skills in evaluating a credit request and reaching a correct decision. Perluence International is large

Determine energy emissions per capita, What is the energy related CO 2 emi...

What is the energy related CO 2 emissions per capita and per $1,000 of GDP? Add the point representing Florida on the Energy CO 2 intensity graph in Appendix. How does it

Balanced mutual fund, Balanced Mutual Fund The mutual fund that objective i...

Balanced Mutual Fund The mutual fund that objective is a balance of stocks & bonds. Balanced funds refer to be less volatile than stock only funds. The return or principal value of

Kan bans in manufacturing enviornment, what are the advantages of dual-card...

what are the advantages of dual-card Kanban system campared to single card in a manufacturing environment

Evacuation of a high rise building - means of escape, Evacuation of a high ...

Evacuation of a high rise building - means of escape: Evacuation of a high rise building is likely to be split into two or more phases.  Initially, when the alarm activates (f

Payback period method, Non-discounted cash flow method, Payback period met...

Non-discounted cash flow method, Payback period method In this method, time value of money is not considered. It takes into account the number of years required to recover the in

Engine protection devices - aircraft engine, Engine protection devices : ...

Engine protection devices : Described below are typical protection devices that will override any excessive demands made on the engine by the pilot or by the control units.

Thermo electric thermometer, how thermoelecteric thermometer is contructed ...

how thermoelecteric thermometer is contructed and how it working

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