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Recent questions in IES Objectives-1
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Which of the following parameters decrease across a normal shock wave?
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2006
ppe
jet-propulsion&compressible-flow
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0
answers
Which of the following assumptions /conditions are true in the case of Rayleigh flow?
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
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ies-objectives-1
2005
ppe
jet-propulsion&compressible-flow
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Which of the following assumptions /conditions are true in the case of Rayleigh flow?
asked
Jan 17, 2018
in
PPE
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chandu
(
215k
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ies-objectives-1
2005
ppe
jet-propulsion&compressible-flow
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Assertion (A): Throttling process for real gases at initial temperature higher than
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Jan 17, 2018
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TD
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chandu
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215k
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ies-objectives-1
2003
td
pure-substance
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The dryness fraction of vapour after throttling process is
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Jan 17, 2018
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TD
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chandu
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215k
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ies-objectives-1
2003
td
pure-substances
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Which of the above statements are correct?
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Jan 17, 2018
in
TD
by
chandu
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215k
points)
ies-objectives-1
2002
td
pure-substances
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With increase of pressure, the latent heat of stream
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Jan 17, 2018
in
TD
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chandu
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215k
points)
ies-objectives-1
2002
td
pure-substances
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Match Lists – I (Process) with List –II (Curves/lines)
asked
Jan 17, 2018
in
TD
by
chandu
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215k
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ies-objectives-1
2001
td
pure-substances
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In which one of the following working substances does the relation
asked
Jan 16, 2018
in
TD
by
chandu
(
215k
points)
ies-objectives-1
2000
td
pure-substances
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0
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The velocity of the aero plane at the same Mach number at an altitude
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2000
ppe
jet-propulsion&compressible-flow
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0
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The Mach number after the shock is
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Jan 16, 2018
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PPE
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chandu
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215k
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ies-objectives-1
2000
ppe
jet-propulsion&compressible-flow
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In turbo prop, the expansion of gases takes place approximately
asked
Jan 16, 2018
in
PPE
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chandu
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215k
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ies-objectives-1
2000
ppe
jet-propulsion&compressible-flow
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With reference to Turbo- jet and Rocket engines, consider the following statements:
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2001
ppe
jet-propulsion&compressible-flow
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In a normal shock in a gas
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Jan 16, 2018
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PPE
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chandu
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215k
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ies-objectives-1
2002
ppe
jet-propulsion&compressible-flow
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For a jet propulsion unit, ideally the ratio of compressor work and turbine work is
asked
Jan 16, 2018
in
PPE
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chandu
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215k
points)
ies-objectives-1
2002
ppe
jet-propulsion&compressible-flow
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A normal shock
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2002
ppe
jet-propulsion&compressible-flow
0
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0
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Match List I (Flow properties) with List II (Mode of changes)
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2002
ppe
jet-propulsion&compressible-flow
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Acoustic velocity in an elastic gaseous medium is proportional to
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2003
ppe
jet-propulsion&compressible-flow
0
votes
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The fluid property that remains unchanged across a normal shock wave is
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2003
ppe
jet-propulsion&compressible-flow
0
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0
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The propulsive efficiency is
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Jan 16, 2018
in
PPE
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chandu
(
215k
points)
ies-objectives-1
2003
ppe
jet-propulsion&compressible-flow
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