This is designed to incentify community members as a proof of contribution token.

Using this You can,Buy courses,Reward others and exchange for real money.

WHITE PAPER COURSES

Real Problems! Real Experts!

Join Our Telegram Channel !

In eduladder you can Ask,Answer,Listen,Earn and Download Questions and Question papers.

Watch related videos of your favorite subject.

Connect with students from different parts of the world.

Apply or Post Jobs, Courses ,Internships and Volunteering opportunity. For FREE

See Our team

Wondering how we keep quality?

Got unsolved questions? Ask Questions

GATE
GMAT
CBSE
NCERT
Career
Interview
Railway
UPSC
NID
NIFT-UG
NIFT-PG
PHP
AJAX
JavaScript
Node Js
Shell Script
Research

Checkout our YouTube channel for video tutorials and learn more about Eduladder.

New updates

Searching for :CareerDate:2022-08-16 12:46:15Done by:Anonymous user(Visitor)Searching for :AJAXDate:2022-08-16 12:05:31Done by:Anonymous user(Visitor)

Searching for :Test closure activities include Date:2022-08-16 11:48:35Done by:Anonymous user(Visitor)

View All

Career 2.0

You might be intrested on below oppertunities Show me All

Posted By:Eduladder

### Similar Questions

**The stagnation pressures at the inlet and exit of a subsonic intake are 100 kPa and 98 kPa, respectively. The pressure recovery of this intake will be ______ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)**

1 Answer

**The stagnation temperatures at the inlet and exit of a combustion chamber are 600 K and 1200 K, respectively GATE-Aerospace Engineering-Question-2012**

1 Answer

**An axial compressor that generates a stagnation pressure ratio of 4.0, operates with inlet and exit stagnation temperatures of 300 K and 480 K, respectively. If the ratio of specific heats (πΎ) is 1.4, the isentropic efficiency of the compressor is (GATE-Aerospace-Engineering-2018 )**

1 Answer

**The theoretical maximum velocity (in m/s) of air expanding from a reservoir at 700 K is __________ (accurate to two decimal places). Specific heat of air at constant pressure is 1005 J/(kg-K). (GATE-Aerospace-Engineering-2018)**

1 Answer

**Air at 50 kPa pressure and 400 K temperature flows in a duct at Mach 3.0. A part of the flow leaks through an opening on the duct wall into the ambient, where the pressure is 30 kPa. The maximum Mach number achieved in the discharge is _______ (accurate to two decimal places). (Ratio of specific heats of air is πΎ=1.4). (GATE-Aerospace-Engineering-2018)**

1 Answer

**The flexural rigidity of the beam (in kN-m^2) is _________________ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)**

1 Answer

**the net hydrostatic force (in kN) on the side face of the tank due to the air and water is ______(GATE-Aerospace-Engineering-2018)**

1 Answer

**Assuming g as 9.81 m/s^2, the power (in MW) needed for it to cruise is _______ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)**

1 Answer

**An axial compressor rotor with 50 % degree of reaction, operates with an axial velocity of 200 m/s. The absolute flow angle at the inlet of the rotor is 22o with reference to the axial direction. If the axial velocity is assumed to remain constant through the rotor, the magnitude of the relative velocity (in m/s) at the rotor exit is __________ (accurate to one decimal place). (GATE-Aerospace-Engineering-2018)**

1 Answer

**The relative velocity of air leaving a straight radial impeller of a centrifugal compressor is 100 m/s. If the impeller tip speed is 200 m/s, for a slip free operation, the absolute velocity (in m/s) at the impeller exit is _________ (accurate to one decimal place). (GATE-Aerospace-Engineering-2018)**

0 Answer

**For a damped single degree of freedom system with damping ratio of 0.1, ratio of two successive peak amplitudes of free vibration is ___________ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)**

1 Answer

**A combustor is operating with a fuel-air ratio of 0.03. If the stoichiometric fuel-air ratio of the fuel used is 0.06, the equivalence ratio of the combustor will be _______ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)**

1 Answer

**A thin-walled tube with external radius of 100 mm and wall thickness of 2 mm, is fixed at one end. It is subjected to a compressive force of 1 N acting at a point on the circumference parallel to its length. The maximum normal stress (in kPa) experienced by the structure is _____________ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)**

1 Answer

**The intake pressure of a diesel engine is 1 bar and pressure at the end of the compression is 34 bar. The adiabatic exponent is 1.3 and the expansion ratio is 7. The diesel cycle efficiency in percentage is __________________ Gate-Agricultural-2016**

1 Answer

**An aircraft with a gross weight of 2000 kg, has a speed of 130 m/s at sea level, where the conditions are: 1 atmosphere (pressure), 288 K (temperature), and 1.23 kg/m^3 (density). The speed (in m/s) required by the aircraft at an altitude of 9000 m, where the conditions are: 0.31 atmosphere, 230 K, and 0.47 kg/m^3, to maintain a steady, level flight is ________ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)**

1 Answer

**A statically-stable aircraft has a πΆπΏπΌ= 5 (where the angle of attack, Ξ±, is measured in radians). The coefficient of moment of the aircraft about the center of gravity is given as πΆπ,π.π=0.05β4πΌ. The mean aerodynamic chord of the aircraft wing is 1 m. The location (positive towards the nose) of the neutral point of the aircraft from the center of gravity is ______ (in m, accurate to two decimal places) (GATE-Aerospace-Engineering-2018)**

1 Answer

**Consider a 20degree half-angle wedge in a supersonic flow at Mach 3.0 at standard sea-level conditions. If the shock-wave angle on the wedge is 36degreee, the Mach number of the tangential component of the flow post-shock is _______ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)**

1 Answer

**Assuming ISA standard sea level conditions (288.16 K, density of 1.225 kg/m^3, g = 9.81 m/s^2, R = 287 J/(kg-K)), the density (in kg/m^3) of air at Leh, which is at an altitude of 3500 m above mean sea level is ________ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)**

1 Answer

**A pitot probe on an aircraft in a steady, level flight records a pressure of 55,000 N/m^2. The static pressure and density are 45,280 N/m^2 and 0.6 kg/m^3, respectively. The wing area and the lift coefficient are 16 m^2 and 2, respectively. The wing loading (in N/m^2) on this aircraft is _________ (accurate to one decimal place). (GATE-Aerospace-Engineering-2018)**

1 Answer

**Gross weight of an airplane is 7000 N, wing area is 16 m^2, and the maximum lift coefficient is 2.0. Assuming density at the altitude as 1.23 kg/m^3, the stall speed (in m/s) of the aircraft is _________ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)**

1 Answer

### Notes

**(GATE-Aerospace-Engineering-2018)**

**Fr. Conceicao Rodrigues College of Engineering, Mumbai**

**GATE- Aerospace Engineering- 2013**

**GATE-Aerospace Engineering-Question paper-2012**

**CE2355 ENVIRONMENTAL AND IRRIGATION ENGINEERING DRAWING**

**Bangalore Institute of Technology, Bangalore**

**Gate 2018 polymer science & engineering**

**Gate-2018-engineering-mathematics**

**(GATE-Agricultural-Engineering-2018)**

**Gate-2018-Mechanical-engineering**

## The stagnation pressures at the inlet and exit of a subsonic intake are 100 kPa and 98 kPa, respectively. The pressure recovery of this intake will be ______ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)

## The stagnation pressures at the inlet and exit of a subsonic intake are 100 kPa and 98 kPa, respectively. The pressure recovery of this intake will be ______ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)

Asked On2019-04-10 14:03:38 by:naikaumprakash

Taged users:

Likes:

Be first to like this question

Dislikes:

Be first to dislike this question

Talk about this Like Dislike

Download question setAnswers(accurate to two decimal places).0.98Likes:

Be first to like this answer

Dislikes:

Be first to dislike this answer

Talk about this Like Dislike

## You might like this video:Network and IP Address

Watch more here

## Watch more videos from this user Here

Learn how to upload a video over here

Lets together make the web is a better placeWe made eduladder by keeping the ideology of building a supermarket of all the educational material available under one roof. We are doing it with the help of individual contributors like you, interns and employees. So the resources you are looking for can be easily available and accessible also with the freedom of remix reuse and reshare our content under the terms of creative commons license with attribution required close.

You can also contribute to our vision of "Helping student to pass any exams"with these.Answer a question:You can answer the questions not yet answered in eduladder.How to answer a questionCareer:Work or do your internship with us.Work with usCreate a video:You can teach anything and everything each video should be less than five minutes should cover the idea less than five min.How to upload a video on eduladder