Propulsion Archives - aerospace answers

Question Cagtegory: Propulsion

All Questions

Filter by

Questions Per Page:

What is the working principle of a turbojet engine ?
What is the working principle of a turbojet engine ?
Airplane design

flight mechanics

thrust

turbojet

Kumar59 Asked on 13th November 2020 in Propulsion.
- 76 views
- 1 answers
- 0 votes
What is thrust reversal ? What are the methods of thrust reversal ?
What is thrust reversal ? What are the methods of thrust reversal ?
thrust

thrust reversal

Kumar59 Asked on 13th July 2020 in Propulsion.
- 204 views
- 1 answers
- 0 votes
What are the advantages of turbojet engine ?
What are the advantages of a turbojet engine ?
Aircraft performance

Airplane design

Supersonic airplanes

thermodynamics

turbojet

Kumar59 Asked on 3rd July 2020 in Propulsion.
- 154 views
- 1 answers
- 0 votes
Find the rate of change of temperature with time.
The temperature distribution at a certain input of time in concrete slab during curing is given by \(T=3x^{2}+3x+16\) where \(x\) …
mech.

thermodynamics

Kisan Kumar Asked on 25th October 2019 in Propulsion.
- 210 views
- 1 answers
- 0 votes
Find the direction of fastest variation in temperature.
The temperature field in a body varies according to the equation \(T(x,y)=x^{3}+4xy\).Find the direction of fastest variation in temperature at …
mech.

thermodynamics

Kisan Kumar Asked on 25th October 2019 in Propulsion.
- 221 views
- 1 answers
- 0 votes
Find the ratio of specific heats.
In case of ideal triatomic gas , What is the ratio of specific heats \(C_p/C_v\)?
Kisan Kumar Asked on 23rd October 2019 in Propulsion.
- 214 views
- 1 answers
- 0 votes
Find the total temperatures at the exit of the air intake and the compressor respectively.
A jet engine is operating at a Mach number of \(0.8\) at an altitude of \(10 \;km\).The efficiency of the …
GATE

Kisan Kumar Asked on 10th October 2019 in Propulsion.
- 194 views
- 1 answers
- 0 votes
Determine the thrust of the turbojet engine.
A turbojet powered aircraft is flying at Mach number \(0.8 \) at an altitude of \(10\; km\).The inlet and exit …
GATE

Kisan Kumar Asked on 10th October 2019 in Propulsion.
- 196 views
- 1 answers
- 0 votes
Find the fuel to air ratio.
The stagnation temperatures at the inlet and exit of a combustion chamber are 600 K and 1200 K ,respectively.If the …
GATE

Kisan Kumar Asked on 8th October 2019 in Propulsion.
- 233 views
- 0 answers
- 0 votes
What will be the ratio for maximum propulsive efficiency?
What is the ratio of flight speed to the exhaust velocity for maximum propulsion efficiency ?
GATE

Kisan Kumar Asked on 2nd October 2019 in Propulsion.
- 203 views
- 1 answers
- 0 votes

Tags

LATEST QUESTIONS

Tags