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Questions by chandu
0
votes
0
answers
Across a normal shock
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2011
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
What is the correct statement regarding normal shock wave in a gas?
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2011
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In Rayleigh flow at subsonic Mach numbers, heat addition
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2011
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In a Rayleigh flow of subsonic compressible flow heating causes
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2011
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Normal shock wave occurs in a one dimensional steady
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2012
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The static temperature is
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2012
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Across the normal shock in a flow
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2012
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
A normal shock wave cannot occur in convergent portion of
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2012
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In a compressible fluid flow field, the Mach number indicates the ratio of
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2012
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Which of the following statements are correct for turbo-prop powered aircrafts?
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Then propulsive efficiency is
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The air fuel ratio at this altitude will be
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Which of the following statements are correct for rockets?
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In an adiabatic flow with friction through a constant area duct, the following phenomenons are predicted:
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Fanno line flow is a flow a constant area duct
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The flow velocity in the convergent section of the nozzle is
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In an isentropic nozzle flow
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Mass flow through the convergent nozzle is maximum when the exit Mach number is
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
When a bluff body moves at supersonic speed in still air
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Stagnation pressure decreases whereas stagnation temperature remains
asked
Jan 17, 2018
in
PPE
ies-objectives-1
2014
ppe
jet-propulsion&compressible-flow
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