Q8
MCQ • 2M
Verbal & Numerical Aptitude
Consider the following functions for non-zero positive integers, p and q. f(p, q) = p × p × p × … … … × pᇣᇧᇧᇧᇧᇧᇧᇤᇧᇧᇧᇧᇧᇧᇥ terms = p; f(p, 1) = p g(p, q) = p⫶⫶⫶(౫౦ ౪ ౪౨ౣ౩) ; g(p, 1) = p Which one of the following options is correct based on the above?
Q9
MCQ • 2M
Verbal & Numerical Aptitude
Four cities P, Q, R and S are connected through one-way routes as shown in the figure. The travel time between any two connected cities is one hour. The boxes beside each city name describe the starting time of first train of the day and their frequency of operation. For example, from city P, the first trains of the day start at 8 AM with a frequency of 90 minutes to each of R and S. A person does not spend additional time at any city other than the waiting time for the next connecting train. If the person starts from R at 7 AM and is required to visit S and return to R, what is the minimum time required?
Q10
MCQ • 2M
Verbal & Numerical Aptitude
Equal sized circular regions are shaded in a square sheet of paper of 1 cm side length. Two cases, case M and case N, are considered as shown in the figures below. In the case M, four circles are shaded in the square sheet and in the case N, nine circles are shaded in the square sheet as shown. What is the ratio of the areas of unshaded regions of case M to that of case N? case M case N
Q16
MCQ • 1M
Incompressible & Compressible Aerodynamics
Consider steady, two-dimensional, incompressible flow over a non-porous flat plate as shown in the figure. For the control volume PQRS, the speed, uஶ, at section PQ is uniform and the speed at section RS is given by u(y) = A ቀ ௬ ቁ , where n is a positive integer. The value of A for which the flow through section PS will vanish is: u 0( ) n yu y A h h
Q35
NAT • 1M
Air-Breathing & Rocket Propulsion
In a single stage turbine, the hot gases come out of stator/ nozzle at a speed of 500 m/s and at an angle of 70 degrees with the turbine axis as shown. The design speed of the rotor blade is 250 m/s at the mean blade radius. The rotor blade angle, 𝛽, at the leading edge is ________ degrees (round off to one decimal place).
Q38
MCQ • 2M
Linear Algebra & Differential Equations
Consider the partial differential equation பమ ப௫మ + பమ ப௬మ = 0 where x, y are real. If f(x, y) = a(x)b(y), where a(x) and b(y) are real functions, which one of the following statements can be true?
Q39
MCQ • 2M
Incompressible & Compressible Aerodynamics
A cylindrical object of diameter 900 mm is designed to move axially in air at 60 m/s. Its drag is estimated on a geometrically half-scaled model in water, assuming flow similarity. Coefficients of dynamic viscosity and densities for air and water are 1.86 × 10ିହ Pa-s, 1.2 kg/m3 and 1.01 × 10ିଷ Pa-s, 1000 kg/m3 respectively. Drag measured for the model is 2280 N. Drag experienced by the full-scale object is ____ N (rounded off to the nearest integer).
Q44
MCQ • 2M
Air-Breathing & Rocket Propulsion
A convergent nozzle fed from a constant pressure, constant temperature reservoir, is discharging air to atmosphere at 1 bar (absolute) with choked flow at the exit (marked as Q). Flow through the nozzle can be assumed to be isentropic. If the exit area of the nozzle is increased while all the reservoir parameters and ambient conditions remain the same, then at steady state
Q45
MCQ • 2M
Structural Mechanics
For a conventional airplane in straight, level, constant velocity flight condition, which of the following condition(s) is/are possible on Euler angles (𝜙, 𝜃, 𝜓), angle of attack (𝛼) and the sideslip angle (𝛽)?
Q47
MSQ • 2M
Air-Breathing & Rocket Propulsion
A rocket operates at an absolute chamber pressure of 20 bar to produce thrust, Fଵ. The hot exhaust is optimally expanded to 1 bar (absolute pressure) using a convergent-divergent nozzle with exit to throat area ratio ቀ ቁ of 3.5 and thrust coefficient, Cி,ଵ =1.42. The same rocket when operated at an absolute chamber pressure of 50 bar produces thrust Fଶ and the thrust coefficient is Cி,ଶ. Which of the following statement(s) is/are correct?
Q48
NAT • 2M
Linear Algebra & Differential Equations
v⃗ = xଷ𝚤̂ + yଷ𝚥̂ + zଷk is a vector field where 𝚤̂, 𝚥̂, k are the base vectors of a cartesian coordinate system. Using the Gauss divergence theorem, the value of the outward flux of the vector field over the surface of a sphere of unit radius centered at the origin is________ (rounded off to one decimal place).
Q50
NAT • 2M
Structural Mechanics
A rotational velocity field in an air flow is given as ˆ ˆV ayi bxj , with a = 10 s-1, b = 20 s-1. The air density is 1.0 kg/m3 and the pressure at (x, y) = (0 m, 0 m) is 100 kPa. Neglecting gravity, the pressure at (x, y) = (6 m, 8 m) is _____ kPa (rounded off to nearest integer).
Q53
NAT • 2M
Incompressible & Compressible Aerodynamics
In a converging duct, area and velocity at section P are 1 m 2 and 15 m/s, respectively. The temperature of the fluid is 300 K. Air flow through the nozzle can be assumed to be inviscid and isothermal. Characteristic gas constant is 287 J/(kg-K) and ratio of specific heats is for air. To ensure that the air flow remains incompressible (Mach number, M ≤ 0.3) in the duct, the minimum area required at section Q is _____ m 2 (rounded off to two decimal places).
Q55
NAT • 2M
Incompressible & Compressible Aerodynamics
A convergent-divergent nozzle with adiabatic walls is designed for an exit Mach number of 2.3. It is discharging air to atmosphere under the conditions indicated in the figure. Flow through the nozzle is inviscid, the characteristic gas constant for air is 287 J/(kg-K), and 𝛾 =1.4. When the reservoir pressure is 25 bar (absolute), and temperature is 300 K, Prandtl- Meyer expansion waves appear at the nozzle exit as shown. The minimum percentage change in the reservoir pressure required to eliminate the wave system at the nozzle exit under steady state is _______%.
Q57
NAT • 2M
Structural Mechanics
Given: The tip deflection and tip slope for a tip loaded cantilever of length L are: ேయ ଷாூ and ேమ ଶாூ, respectively, where N is the tip force and EI is the flexural rigidity. A cantilever PQ of rectangular cross-section is subjected to transverse load, F, at its mid-point. Two cases are considered as shown in the figure. In Case I, the end Q is free and in Case II, Q is simply supported. The ratio of the magnitude of the maximum bending stress at P in Case I to that in Case II is ________ (rounded off to one decimal place).
Q65
NAT • 2M
Structural Mechanics
A multistage axial compressor takes in air at 1 atm, 300 K and compresses it to a minimum of 5 atm. The mean blade speed is 245 m/s and work coefficient, ∆ഇ is 0.55 for each stage. For air, use C =1005 J/(kg-K), R = 287 J/(kg-K) and γ = 1.4. If the compression is isentropic, the number of stages required is ___________ (rounded off to the next higher integer).