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Questions by chandu
0
votes
0
answers
In a normal shock in a gas
asked
Jan 16, 2018
in
PPE
ies-objectives-1
2002
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
For a jet propulsion unit, ideally the ratio of compressor work and turbine work is
asked
Jan 16, 2018
in
PPE
ies-objectives-1
2002
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
A normal shock
asked
Jan 16, 2018
in
PPE
ies-objectives-1
2002
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Match List I (Flow properties) with List II (Mode of changes)
asked
Jan 16, 2018
in
PPE
ies-objectives-1
2002
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Acoustic velocity in an elastic gaseous medium is proportional to
asked
Jan 16, 2018
in
PPE
ies-objectives-1
2003
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The fluid property that remains unchanged across a normal shock wave is
asked
Jan 16, 2018
in
PPE
ies-objectives-1
2003
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The propulsive efficiency is
asked
Jan 16, 2018
in
PPE
ies-objectives-1
2003
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The efficiency of jet engine is
asked
Jan 16, 2018
in
PPE
ies-objectives-1
2003
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The propulsive efficiency of a turbojet aircraft approaches 100% when the thrust approaches
asked
Jan 16, 2018
in
PPE
ies-objectives-1
2003
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The use of turbo- prop engine is limited to
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1999
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Mach angle $\alpha$ and mach number M are related as:
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1999
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Propulsion efficiency of propeller drive aircraft is
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1998
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
A bypass jet engine gives a better propulsive efficiency and better fuel economy
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1998
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Which of the following pairs of engine and performance/ characteristic is/.are correctly matched?
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1998
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The propulsive efficiency is
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1999
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The mach number is less than 1 at a point where the entropy is
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1999
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The mach number of the flow corresponding to the maximum entropy will be
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1999
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
A typical value of this critical Mach number is of the order of
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1995
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Propulsion efficiency of a jet engine is given by
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1995
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
As compare to turbo- prop, a turbo- jet
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1995
ppe
jet-propulsion&compressible-flow
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