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GATE 2021 Aerospace Engineering Question Paper-Propulsion & GasDynamics Solutions | GATE AE Coaching 

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Комментарии : 18   
@bitians2270
@bitians2270 Год назад
Thank you bhai
@iitiansgateclasses
@iitiansgateclasses Год назад
Thanks
@benjin3385
@benjin3385 Год назад
Regarding question 33, sir said that changing reference frame doesnt change static properties. Then will p2'=p2, T2'=T2? these are downstream conditions in both the cases. Will they be same?
@AMITKUMAR-fo4lx
@AMITKUMAR-fo4lx 11 месяцев назад
I think this question has not good explanation...it can be more good than this
@akshayhegde5286
@akshayhegde5286 11 месяцев назад
Yes you are right. Since, across the shock wave flow properties jump, static properties also jump with similar magnitude. Here, static properties are same because those defines the state of the gas and we are considering the same fluid, the properties does not change with coordinate transformation. Whereas, total properties change because they are defined quantities, if you add dynamic part contributions in moving fluid such as transformed system here, total properties also change. Note that, total temperature across the moving shock is not constant eventhough process is adiabatic is because the flow process is unsteady in case of moving shock systems.
@AMITKUMAR-fo4lx
@AMITKUMAR-fo4lx 11 месяцев назад
Q8. Isp=F/weight flow rate, but in question Isp given interms of F/ mass flow rate
@akshayhegde5286
@akshayhegde5286 11 месяцев назад
Yes, you are right. Here it seems the question is using different unit for specific impulse. Specific impulse has unit of seconds. In question they have m/s and that is the unit of specific thrust. Simple dimensional analysis can give you correct answer. Remember, these quantities are defined quantities and author can define in his own way as long as they provide the correct dimensions gor their definition. Here it is given in m/s and hence the definition modifies to Thrust/mass flow rate instead of Thrust/weight flow rate.
@kumaaar3480
@kumaaar3480 2 года назад
Sir how u got h04=1120657.5 J/kg
@bitians2270
@bitians2270 Год назад
Bhai I'm preparing for gate 2024 i don't know where to start can you help me
@iitiansgateclasses
@iitiansgateclasses Год назад
You can join any of IGC's course...or start with basic subjects like mechanics, Fluid, Thermo, SOM n mathematics...then start with core subjects
@bitians2270
@bitians2270 Год назад
@@iitiansgateclasses what is IGC how much it cost
@iitiansgateclasses
@iitiansgateclasses Год назад
@@bitians2270 For more GATE Aerospace courses for GATE 2024 Visit 👉 www.iitiansgateclasses.com/
@bitians2270
@bitians2270 Год назад
@@iitiansgateclasses it is asking to register how much will they ask to pay please reply
@iitiansgateclasses
@iitiansgateclasses Год назад
@@bitians2270 you can look into courses available n fee for same..
@AMITKUMAR-fo4lx
@AMITKUMAR-fo4lx 11 месяцев назад
Q33. Option 4 is wrong Po1'
@akshayhegde5286
@akshayhegde5286 11 месяцев назад
Nope, p01 < p01' Here, in moving shock system, static and stagnation properties are same for fluid ahead of the shock wave since, gas is stagnant until it encounters the shock.
@AMITKUMAR-fo4lx
@AMITKUMAR-fo4lx 11 месяцев назад
@@akshayhegde5286 but in original option you change the last quantity and option d is right but show you show different than original
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