Air-fuel ratio in a jet engine will be of the order of 0.41736111111111 2.5006944444444 0.62569444444444 0.83402777777778 TRUE ANSWER : ? YOUR ANSWER : ?
The mass of gas turbine per kW developed is about ________ as that of an I.C. engine. One sixth One-half Same One fourth TRUE ANSWER : ? YOUR ANSWER : ?
The absolute pressure of air at the outlet of a compressor is called Critical pressure Discharge pressure Back pressure None of the listed here TRUE ANSWER : ? YOUR ANSWER : ?
If the clearance ratio for a reciprocating air compressor is 'K', then its volumetric efficiency is given by 1 - k + k (p₁/p₂)1/n 1 - k + k (p₁/p₂) n- 1/n 1 + k - k (p₂/p₁) n-1/n 1 + k - k (p₂/p₁)1/n TRUE ANSWER : ? YOUR ANSWER : ?
The indicated work per unit mass of air delivered is Greatly affected by clearance volume Not affected by clearance volume Directly proportional to clearance volume Inversely proportional to clearance volume TRUE ANSWER : ? YOUR ANSWER : ?
The maximum propulsion efficiency of a turbojet is attained at around following speed 550 km/hr 1050 km/hr 1700 km/hr 2400 km/hr TRUE ANSWER : ? YOUR ANSWER : ?
In which case the air-fuel ratio is likely to be maximum? 4-stroke petrol engine Multi cylinder engine Gas turbine 4-stroke diesel engine TRUE ANSWER : ? YOUR ANSWER : ?
A closed cycle gas turbine works on Joule cycle Rankine cycle Ericsson cycle Carnot cycle TRUE ANSWER : ? YOUR ANSWER : ?
A gas turbine used in air craft should have High h.p. and low weight High speed and high h.p. Low weight and small frontal area Small frontal area and high h.p. TRUE ANSWER : ? YOUR ANSWER : ?
Aeroplanes employ following type of compressor None of these Centrifugal Radial flow Axial flow TRUE ANSWER : ? YOUR ANSWER : ?