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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.
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
what is rigidity modulus?mention its units?
Electrical ice protection systems: Electrical ice protection systems are used on most turbo-props. Resistance wire heater elements are embedded in rubber and cemented from the
Measurement of thermocouple voltage The voltage is typically only a few millivolts and should be measured using a high impedance system. If an amplifier is used, must also have
how can we find local attraction correction?
explain any two finishing processes in detail with neat diagram
Procedures for starting and ground running: Before starting and ground running any gas turbine powered aircraft, several considerations must be taken into account. The first an
centralized organization
dhpl is the firm situated in faridabad,its ending year on 31st march 2009 ,1000million asset base rs.650 million & the net profit of the company was 76 milloin the managmnt of the
Trim tabs are small flaps attached to the rear of the main control surfaces. They can be adjusted the pilot to reduce the force required to hold the control surface in its deflecte
what are the components, applications, benefits and drawbacks of control engineering?????
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