Pitot intakes - aircraft maintenance , Other Engineering

Assignment Help:

Pitot intakes:

This intake is suitable for subsonic or low supersonic speeds. Examples, 707, 747, A300B, Tristar, etc. The intake is usually short and is very efficient because the duct inlet is located directly ahead of the engine compressor. As the duct length increases, the risk of small airflow disturbances and pressure drop is increased. This inlet makes maximum use of ram effect until sonic speed is approached when efficiency falls due to shock wave formation at the intake lip. Pitot inlets can however suffer from inlet turbulences at high angles of attack and/or at low speeds.

1554_Pitot intakes.png

The pitot type intake can be used for engines that are mounted in pods or in the wings although the latter sometimes requires a departure from the circular cross section due to the wing thickness

 


Related Discussions:- Pitot intakes - aircraft maintenance

Project report, I need help for my project report plz. > Precast concrete p...

I need help for my project report plz. > Precast concrete panels manufactured in factory environments and rapidly cured using steam are being used for the walls of shallow foundati

Physical chemistry, can you answer some problem from physical chemistry wit...

can you answer some problem from physical chemistry with a detailed approach why and how one should choose the steps in solving them.These are just random question that I have no c

Aerofoil aerodynamics – low speed flows, We now have some idea about what m...

We now have some idea about what models are available to simulate the flow over an aerofoil, and also how to use the Hanley package to apply these methods. Keep referring to you

Biomechanics, i have homework in my biomechanics class

i have homework in my biomechanics class

Dischage rate, stuck on a project that requires 5 outputs with 6 inputs and...

stuck on a project that requires 5 outputs with 6 inputs and all formulas

Hysteresis, hysteresis loss least epends on

hysteresis loss least epends on

Thrust calculation- aeronautical engineering , Thrust calculation: The ...

Thrust calculation: The amount of thrust produced depends upon two things:- The MASS of air which is moved rearwards in a given time, the ACCELERATION imparted to the air.It

Aerodynamics-flow model diagram , We will need to use several different flo...

We will need to use several different flow models as we go along. It is crucial to understand the simplifications used to obtain these models because these limit the validity of th

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