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GATE Aerospace - Aircraft Propulsion - Lecture 02 - Axial flow Compressor (AFC)

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This lecture series by GOODWILL GATE2IIT will cover complete GATE AEROSPACE syllabus. The present module will be covering Aircraft Propulsion. The series of lectures are intended to focus directly on GATE concepts and provide quality education to students.
All GATE problems will be solved and extra questions will be provided for students to practice along with the solution.
This lecture will cover Working and construction of Axial flow Compressor (AFC)

Опубликовано:

20 июл 2017

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Комментарии : 23

@chickyapoo1913 7 лет назад

Awesome explanation...I understood the concept clearly. Thank u sir..:)

@a.dineshkumar47 2 года назад

Awesome explanation . And I clearly understood about the topic so well great lecture thanks 🙂 again . I will see lot section with more curiosity👍

@MYagna1981 7 лет назад

thank for explanation sir

@MOHANRAJ-wt6hl 6 лет назад

Sir your explanation is very clear ,,,thanking you 😊

@ashishdushing6665 6 лет назад

Awesome

@mohdaamirkhanlucknow5208 6 лет назад

Sir your explanation is very clear. Please upload more video

@niravfatekar4691 3 года назад

Sir please upload more videos . I understand very well in these lecture

@chandrashekhar-oq8io 4 года назад

Sir please explain velocity triangle also.. Your explanation is excellent.. Thank u

@maramsaimanikanta5178 6 лет назад

Nice and understandable explanation ....when u r gng to upload more videos??

@umeshrana8402 2 года назад

Sir please uploaded all videos...please sir

@tanishqjain3019 7 лет назад

when wil you upload third lecture sir

@jaypanchal1997 6 лет назад

Sir please upload more and more videos.....

@sakshikhiroriya9607 10 месяцев назад

where can we find continuation lectures ? Reply

@sangitduniya7130 7 лет назад

please start structures. thankyou

@summaiyanajeem4434 6 лет назад

sir i am unable to find..3lecture...plzz help me out..

@premnaik4752 2 года назад

where can we find continuation lectures ?

@astrobhas3144 5 лет назад

Sir when will u upload 3 rd lecture?

@MrRejuR 3 года назад

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?

@smohammedkaif6037 3 года назад

where is lecture 3.....?

@krishnashekhawat6225 6 лет назад

Provide all videos of propulsion for gate

@MYagna1981 7 лет назад

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

@gateaerospace 7 лет назад

@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.....

@MrRejuR 3 года назад

@@gateaerospace difficult to understand