Please share the answer for the question... Why the length of the blades are decreasing? Which pressure is increasing? Which pressure we need? Compressor width and turbine width difference.. Why?
stagnation pressure -constant,static pressure- increases as no of stagings increases,why convergent for compressor blades ,because to increase density of air so that pressure rise will be more
@Sai Krishna - Stagnation pressure increases in Rotor blades, because energy is supplied from turbine in rotor section, where as static pressure increases in both the rotor as well as stator blades, unless degree of reaction is zero. If we take friction into account, there will be actually reduction is stagnation pressure in stator blades. If you neglect friction stagnation preesure remains constant in stator blades. This is same for all the stages. Hope this answer helps.....
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Awesome explanation . And I clearly understood about the topic so well great lecture thanks 🙂 again . I will see lot section with more curiosity👍
Sir your explanation is very clear ,,,thanking you 😊
Sir please uploaded all videos...please sir
where can we find continuation lectures ?
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Awesome explanation...I understood the concept clearly. Thank u sir..:)
Sir please upload more videos . I understand very well in these lecture
where can we find continuation lectures ?
Sir your explanation is very clear.
Please upload more video
where is lecture 3.....?
thank for explanation sir
Sir please explain velocity triangle also..
Your explanation is excellent..
Thank u
Nice and understandable explanation ....when u r gng to upload more videos??
when wil you upload third lecture sir
Awesome
Please share the answer for the question... Why the length of the blades are decreasing?
Which pressure is increasing?
Which pressure we need?
Compressor width and turbine width difference.. Why?
sir i am unable to find..3lecture...plzz help me out..
Sir when will u upload 3 rd lecture?
stagnation pressure -constant,static pressure- increases as no of stagings increases,why convergent for compressor blades ,because to increase density of air so that pressure rise will be more
@Sai Krishna - Stagnation pressure increases in Rotor blades, because energy is supplied from turbine in rotor section, where as static pressure increases in both the rotor as well as stator blades, unless degree of reaction is zero. If we take friction into account, there will be actually reduction is stagnation pressure in stator blades. If you neglect friction stagnation preesure remains constant in stator blades. This is same for all the stages.
Hope this answer helps.....
@@gateaerospace difficult to understand
please start structures.
thankyou
Provide all videos of propulsion for gate
Sir please upload more and more videos.....