Question Category: Mechanical Engineering

Questions › Category: Mechanical Engineering
Filter:AllOpenResolvedClosedUnanswered
The combustion efficiency of a gas turbine using perfect combustion chamber is of the order of
OpenVideRime asked 3 years ago • 
161 views0 answers0 votes
It is not possible to use closed gas turbine cycle in aeronautical engines because
OpenVideRime asked 3 years ago • 
169 views0 answers0 votes
In open cycle turbojet engines used in military aircraft, reheating the exhaust gas from the turbine by burning, more fuel is used to increase the
OpenVideRime asked 3 years ago • 
181 views0 answers0 votes
The material commonly used for air craft gas turbine is
OpenVideRime asked 3 years ago • 
189 views0 answers0 votes
A jet engine has
OpenVideRime asked 3 years ago • 
180 views0 answers-1 votes
The volume of air delivered by the compressor is called
OpenVideRime asked 3 years ago • 
167 views0 answers0 votes
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is
OpenVideRime asked 3 years ago • 
193 views0 answers0 votes
Efficiency of gas turbine is increased by
OpenVideRime asked 3 years ago • 
178 views0 answers0 votes
The inlet pressure is always ________ the discharge pressure.
OpenVideRime asked 3 years ago • 
139 views0 answers0 votes
Gas turbine blades are given a rake
OpenVideRime asked 3 years ago • 
161 views0 answers0 votes
1…4041424344…187