ASHCHARYA BANSAL

Good Morning 🌄 “A fresh morning is life’s silent message, you still have time to achieve your dreams.”

IIT KANPUR

IISC

IISC

The BARC interviews have already started. If any of you have appeared for the remaining interviews, please share your interview experience on my WhatsApp number 9205326638 Thank you so much.

IIT MADRAS

IIT BOMBAY

Sometimes life doesn’t make sense in the moment. Delays, failures, heartbreaks, and unexpected changes can feel unfair. But maybe… some things are not happening to you, they are happening for you. God’s plan is often clearer in hindsight than in the present. Keep faith. Keep working. Keep moving forward. What is meant for you will find you at the right time. ✨

The Indian Air Force introduces GATE score based entry into the Ground Duty (Technical) Branch. Direct shortlisting for AFSB based on GATE score. This is in addition to entry through AFCAT.

Power plant Chapter 3 Qno 6 Solution Statement 1 and 2 (Incorrect): Stalling in axial compressors is typically categorized as positive and negative stalling based on the angle of attack. Flow separation on the suction side is generally associated with an increase in the angle of attack beyond a critical point, leading to a loss of lift and often referred to as positive stalling. Conversely, flow separation on the pressure side, which can occur at very low or negative angles of attack, is sometimes referred to as negative stalling, but the primary concern in compressor operation is positive stalling due to high angles of attack. The definitions provided in statements 1 and 2 are reversed from the commonly accepted terminology in compressor aerodynamics. Statement 3 (Correct): Rotating stall is a phenomenon where localized regions of stalled flow rotate around the annulus of the compressor. This rotating pattern disrupts the steady flow, leading to significant aerodynamic losses and reduced efficiency, thereby decreasing the effectiveness of the compressor. Statement 4 (Correct): Large-scale stalling, which can lead to surge, results in a significant drop in the delivery pressure and can cause flow reversal in the compressor. Surge is an unstable phenomenon characterized by oscillations in flow and pressure, and the complete breakdown of steady flow can lead to flow reversal, where air flows backward through the compressor

Yes sir Interview date :29 march 2023 Reporting time 9 am There were total 12 candidates and only 1 Interview panel having 5 members ( all are drdo scientist) none are IIT Prof Chairman 1.Introduction 2. Since I was working in AAI as an ATC , asked me why u want to leave such a prestigious job 3. Why you want to join DRDO since AAI is also aPSU 4. Tell me something about drdo. I told about that and also mentioned some missile names like brahmos Now next question was from here. Chairman shift me to member 1 telling me that he is the scientis looking after bhrahmos. Member 1 : what do u know about brahmos? What is genset? Did u studied basic electrical engineering in 1 st year? I told yes Then asked me to tell what is genset? Draw sfd and bmd of axle of vehicle? What are the types of diesel engine? Not IC ENGINE Member 2: tell me about cruise missile What is the speed of missile? Just tell me in terms of mach number? Can speed of missile be subsonic also? What is the speed of sound? Member 3: asked me only one or two questions related to AIRCRAFT since I was in ATC What type of fuel is used in aircraft? What type of engine in aircraft? Member 4: tell me about launching pad? How we can design launching pad? Material of launching pad? What is co ordinates? What is space? Chairman : Told me that time is running out I will now ask you only one last question It is about shear stress related to their project which was going on in drdo They provided me with hardly some time to think So I couldnot be able to think about that. Then he told thank u amit Total duration was about approx 40 minutes On that day everbodys interview was going for around 40 minutes.

Previous year HPCL PAPER LINK https://drive.google.com/file/d/1aVjaFl61TF-YPfDTEY50JxlvyLCGA9W1/view?usp=drivesdk https://drive.google.com/file/d/1-zODv-AmT8qvpuPoYwwrqkxBb1nUQX4t/view?usp=drivesdk https://drive.google.com/file/d/1z21ZP4cRAZ96eOhyO8Xa9nom0xLQfhiA/view?usp=drivesdk https://drive.google.com/file/d/1F4KD48Np-j07k32RWtmKD5AObYIN8-d_/view?usp=drivesdk https://drive.google.com/file/d/1kq0iI4NGJhuLQ7re5Am_WHldUzqRYjjm/view?usp=drivesdk Best Wishes 😊😊😊😊✌️✌️✌️✌️