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Questions by chandu
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
Under which one of the following sets of conditions will a supersonic compressor have the highest efficiency?
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1995
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The flight mach number of the aircraft is
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1995
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In normal shock in a gas, the
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1998
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The prime parameter causing change of state in a Fanno flow is
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1998
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In the case of Fanno line flow, in the subsonic region friction causes
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1997
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Compared to a turbo- jet engine, a turbo- prop engine has a higher power for take – off
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1997
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Rayleight line flow is a flow in a constant area duct
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1997
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Fanno line flow is a flow in a constant area duct
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1997
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Consider the following statements about a rocket engine:
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1997
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
For oblique shock, the downstream mach number
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1997
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Across the normal shock, the fluid properties change in such a manner that the
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Only rocket engines can be propelled to space because
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Consider the following statements relating to rocket engines:
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In a turbo- jet engine, subsequent to heat addition to compressed air, to get the power output
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In a turbo- jet engine, subsequent to heat addition to compressed air, to get the power output
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In open cycle turbo- jet engines used in
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In the subsonic range the propulsive efficiency of a rocket less than
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1995
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The propulsive efficiency of the units is
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1998
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In a turbo- jet engine, thrust may be increased by
asked
Jan 16, 2018
in
PPE
ies-objectives-1
1998
ppe
jet-propulsion&compressible-flow
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