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MCQOPTIONS
This section includes 2374 Mcqs, each offering curated multiple-choice questions to sharpen your Embedded Systems knowledge and support exam preparation. Choose a topic below to get started.
| 401. |
What was the original design of Jerome H. Lemelson which he patented for FMS (Flexible manufacturing system)? |
| A. | Robot based system |
| B. | Conveyer |
| C. | Motor based pulley |
| D. | Shredder |
| Answer» B. Conveyer | |
| 402. |
Anyone can operate FMS (Flexible manufacturing system). |
| A. | True |
| B. | False |
| Answer» C. | |
| 403. |
Flexible manufacturing system (FMS) lowers the company’s production cost. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 404. |
Which is a false statement on FMS (Flexible manufacturing system)? |
| A. | Accuracy in the final goods produced is high |
| B. | The cost of production is less |
| C. | Quality and quantity of produced goods can be changed easily |
| D. | The cost of initial setup is less due to less labour cost |
| Answer» E. | |
| 405. |
What is done in make-to-order production? |
| A. | Production is ordered by the owner |
| B. | Regular production |
| C. | Production stops due to less order |
| D. | Production is done according to customer requirements |
| Answer» E. | |
| 406. |
When did Jerome H. Lemelson set up his factory based on FMS (Flexible manufacturing system)? |
| A. | Early 1950’s |
| B. | Early 1940’s |
| C. | Late 1940’s |
| D. | Late 1960’s |
| Answer» E. | |
| 407. |
Who developed FMS (Flexible manufacturing system)? |
| A. | Jerome H. Lemelson |
| B. | Charles Wheatstone |
| C. | Charles manes |
| D. | Samuel Hunter Christie |
| Answer» B. Charles Wheatstone | |
| 408. |
At what temperature is the vapor condensed is freeze dryer? |
| A. | -20oc |
| B. | -30oc |
| C. | -40oc |
| D. | -60oc |
| Answer» E. | |
| 409. |
What is screw dryer suitable for? |
| A. | Very thick slurries |
| B. | Materials which are heat sensitive |
| C. | Free flowing granular materials |
| D. | Free flowing slurries |
| Answer» D. Free flowing slurries | |
| 410. |
Which of the following is not an indirect heat batch dryer? |
| A. | Jacketed-shelf dryer |
| B. | Agitated pan dryer |
| C. | Conical vacuum dryer |
| D. | Drum dryer |
| Answer» E. | |
| 411. |
Corrosion in the pump is developed due to _______ |
| A. | Pressure of air |
| B. | Fluid properties |
| C. | Draft tube |
| D. | Tank dimensions |
| Answer» C. Draft tube | |
| 412. |
NPSHr is determined by using ______ |
| A. | Pump pressure |
| B. | PumpLinx |
| C. | Heat transfer |
| D. | Chemical energy |
| Answer» C. Heat transfer | |
| 413. |
What is positive suction head? |
| A. | Draft tube is above |
| B. | Pump pressure is above |
| C. | Liquid level is above |
| D. | Turbine head is above |
| Answer» D. Turbine head is above | |
| 414. |
When the NPSH is low, it leads to ________ |
| A. | Breaking |
| B. | Wear |
| C. | Corrosion |
| D. | Cavitation |
| Answer» E. | |
| 415. |
What is the dimension for Darcy’s friction factor? |
| A. | kg/m |
| B. | N/mm |
| C. | kg |
| D. | Dimensionless |
| Answer» E. | |
| 416. |
In hydraulic head, NPSH is used for the analysis of __________ |
| A. | Adiabatic expansion |
| B. | Priming |
| C. | Wear |
| D. | Cavitation |
| Answer» E. | |
| 417. |
The CpG islands generally consist of how many GC bases? |
| A. | 100 |
| B. | Less than 100 |
| C. | More than 1000 |
| D. | 1000 |
| Answer» E. | |
| 418. |
What is the maximum limit (ppm) for Alkali Carbonates and Bicarbonates in the water? |
| A. | 500 |
| B. | 1000 |
| C. | 2000 |
| D. | 1500 |
| Answer» C. 2000 | |
| 419. |
What is the maximum limit (ppm) for turbidity in water? |
| A. | 500 |
| B. | 1000 |
| C. | 2000 |
| D. | 1500 |
| Answer» E. | |
| 420. |
What is the maximum limit (ppm) for SO3 in water? |
| A. | 500 |
| B. | 1000 |
| C. | 2000 |
| D. | 1500 |
| Answer» C. 2000 | |
| 421. |
There is necessary to minimize the use of salt water in RCC. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 422. |
What is the permissible limits for construction of chlorides in water for RCC work? |
| A. | 200mg/l |
| B. | 2000mg/l |
| C. | 1000mg/l |
| D. | 500mg/l |
| Answer» D. 500mg/l | |
| 423. |
Which of the following cloud storage is consumed by file sharing software? |
| A. | Managed |
| B. | Unmanaged |
| C. | UnAvailable |
| D. | All of the mentioned |
| Answer» C. UnAvailable | |
| 424. |
Which of the following storage option is available for managed storage? |
| A. | formatting |
| B. | partitioning |
| C. | replicating data |
| D. | all of the mentioned |
| Answer» E. | |
| 425. |
Which of the following cloud storage involves the provisioning of a raw virtualized disk? |
| A. | Managed |
| B. | Unmanaged |
| C. | Unavailable |
| D. | All of the mentioned |
| Answer» B. Unmanaged | |
| 426. |
Which of the following storage is presented to a user as if it is a ready-to-use disk drive? |
| A. | Managed |
| B. | Unmanaged |
| C. | Unavailable |
| D. | None of the mentioned |
| Answer» C. Unavailable | |
| 427. |
Which of the following presents the developer with their own APIs? |
| A. | VMWare vCloud |
| B. | Racksapce Cloud Servers |
| C. | RimuHosting |
| D. | Racksapce Cloud Servers |
| Answer» E. | |
| 428. |
Applications using managed cloud storage are __________ as a Service Web service. |
| A. | Infrastructure |
| B. | Platform |
| C. | Service |
| D. | All of the mentioned |
| Answer» B. Platform | |
| 429. |
Which of the following is cross-platform API based on generalizing the major cloud vendors APIs? |
| A. | Deltacloud |
| B. | Simple Cloud API |
| C. | Design Cloud |
| D. | All of the mentioned |
| Answer» E. | |
| 430. |
Which of the following mechanisms are contained by Cloud API for accessing cloud services? |
| A. | Abstraction |
| B. | Authentication |
| C. | Replication |
| D. | All of the mentioned |
| Answer» C. Replication | |
| 431. |
At high Q values, the angular balance condition is _________ |
| A. | satisfied |
| B. | not satisfied |
| C. | independent of Q factor |
| D. | partially affected |
| Answer» C. independent of Q factor | |
| 432. |
Commercial Maxwell bridges measures _________ |
| A. | inductances in the range of 1 to 1000H |
| B. | capacitances in the range of 10mF to 1F |
| C. | resistances in the range of 0.001 Ω to 1Ω |
| D. | power in the range of 1W to 50MF |
| Answer» B. capacitances in the range of 10mF to 1F | |
| 433. |
How can R1 be scaled? |
| A. | by using a scale |
| B. | by using an ohmmeter |
| C. | by calibration |
| D. | by using a galvanometer |
| Answer» D. by using a galvanometer | |
| 434. |
What is the significance of the balance equation on losses? |
| A. | independent of losses in inductance |
| B. | independent of losses in capacitance |
| C. | independent of losses in resistance |
| D. | independent of losses in the circuit |
| Answer» B. independent of losses in capacitance | |
| 435. |
In Steady level unaccelerated flight, lift is equal to weight. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 436. |
A jet engine is designed to operate at endurance of 12hrs. If weight fraction is 1.6 and jet engine has tsfc C as 0.00021 per second then, find at which lift to drag ratio that can satisfy above criteria. |
| A. | 19.3 |
| B. | 18 |
| C. | 12 |
| D. | 12.6 |
| Answer» B. 18 | |
| 437. |
A prop driven aircraft has propeller efficiency of 0.92 and C as 0.000745 1/m. If lift to drag ratio is 14 and weight fraction as 1.145 then, find range of the propeller driven aircraft. |
| A. | 2340.95m |
| B. | 2340.5miles |
| C. | 2340km |
| D. | 2500miles |
| Answer» B. 2340.5miles | |
| 438. |
A propeller aircraft has wing loading of 30 unit and is operating with density of 1.21 unit. Determine velocity for maximum loiter. Consider K/CD0 as 0.1. |
| A. | 3unit |
| B. | 5unit |
| C. | 9unit |
| D. | 10unit |
| Answer» B. 5unit | |
| 439. |
An aircraft has maximum lift to drag ratio of 15. If we want to fly aircraft for best range then, find the best value of aerodynamic efficiency to achieve above mentioned result. |
| A. | 12.9 |
| B. | 13.5 |
| C. | 15 |
| D. | 12.1 |
| Answer» B. 13.5 | |
| 440. |
Find instantaneous range of a jet propelled aircraft if lift to drag ratio is 12 and weight fraction at cruise W1/W0 is 1.9. Consider cruise speed of 120m/s and SFC of 0.00161 per second. |
| A. | 574km |
| B. | 574m |
| C. | 574miles |
| D. | 574ft |
| Answer» B. 574m | |
| 441. |
Find the value of lift coefficient to ensure power required minimum condition for cruise if CD0/K is given as 0.480. |
| A. | 1.2 |
| B. | 2.1 |
| C. | 1.7 |
| D. | 7.5 |
| Answer» B. 2.1 | |
| 442. |
Determine the value of drag at which we can have minimum power if given reference area is 10m2 and zero lift drag coefficient is 0.5. Consider q as 120Pa. |
| A. | 2400N |
| B. | 1.25 |
| C. | 9.85 |
| D. | 4500 KN |
| Answer» B. 1.25 | |
| 443. |
If power required at sea level altitude is 2005W then, determine power required at altitude at which density ratio is 0.9. |
| A. | 2.113KW |
| B. | 211115W |
| C. | 2354W |
| D. | 500W |
| Answer» B. 211115W | |
| 444. |
An aircraft is operating with CL of 1.5 and has power required of 120W. If we want to reduce the power required by half then, find the value of CL at this power required condition. Consider steady level flight. |
| A. | 2.38 |
| B. | 1.946 |
| C. | 9.45 |
| D. | 5.59 |
| Answer» B. 1.946 | |
| 445. |
An aircraft has L/D as 12 and thrust required at this value is 100N. Now if L/D has doubled then what will be the new thrust required? |
| A. | 50N |
| B. | 500N |
| C. | 100 N |
| D. | 12.5N |
| Answer» B. 500N | |
| 446. |
Calculate how much power will require to maintain cruise speed of 120 m/s if thrust required is 1KN. Consider steady level flight. |
| A. | 120KW |
| B. | 110N |
| C. | 120N |
| D. | 129W |
| Answer» B. 110N | |
| 447. |
Find the P.I for the given Differential Equation.\(16x^2 \frac{d^2 y}{dx^2}+(2x+4) \frac{dy}{dx}+4x(x+4) \frac{d^2 y}{dx^2}+2y=cos(log(2x+4))\) |
| A. | \(\frac{1}{4}×(-sin(log(2x+4))+cos(log(2x+4)))\) |
| B. | \(\frac{1}{4}×(-sin(log(2x+4))-cos(log(2x+4)))\) |
| C. | \(\frac{1}{2}×(-sin(log(2x+4))-cos(log(2x+4)))\) |
| D. | \(\frac{1}{2}×(-sin(log(2x+4))+cos(log(2x+4)))\) |
| Answer» C. \(\frac{1}{2}×(-sin(log(2x+4))-cos(log(2x+4)))\) | |
| 448. |
Solve this Differential Equation to find its General Solution.\((x+3)\frac{d^2y}{dx^2}+2 \frac{dy}{dx}+\frac{y}{(x+3)}=4\) |
| A. | \(\frac{4x}{3}+2+\frac{1}{(x+3)}×c_1cos(\frac{\sqrt{3}}{2} log(x+3))+c_2sin(\frac{\sqrt{3}}{2} log(x+3))\) |
| B. | \(\frac{4x}{3}+4+\frac{1}{(x+3)}×c_1cos(\frac{\sqrt{3}}{2} log(x+3))+c_2sin(\frac{\sqrt{3}}{2} log(x+3))\) |
| C. | \(x+4+\frac{1}{(x+3)}×c_1cos(\frac{\sqrt{3}}{2} log(x+3))+c_2sin(\frac{\sqrt{3}}{2} log(x+3))\) |
| D. | \(\frac{2x}{3}+4+\frac{1}{(x+3)}×c_1cos(\frac{\sqrt{3}}{2} log(x+3))+c_2sin(\frac{\sqrt{3}}{2} log(x+3))\) |
| Answer» C. \(x+4+\frac{1}{(x+3)}×c_1cos(\frac{\sqrt{3}}{2} log(x+3))+c_2sin(\frac{\sqrt{3}}{2} log(x+3))\) | |
| 449. |
Find the Continuous Function and Particular Integral for the given differential equation.\((2x+3)\frac{dy}{dx}-3y=8x\) |
| A. | \(c_1(2x+3)^\frac{5}{2}, -4(2x+3)-4\) |
| B. | \(c_1(2x+3)^\frac{3}{2}, -2(2x+3)-4\) |
| C. | \(c_1(2x+3)^\frac{3}{2}, -4(2x+3)-4\) |
| D. | \(c_1(2x+3)^\frac{3}{2}, -4(2x+3)-4\) |
| Answer» D. \(c_1(2x+3)^\frac{3}{2}, -4(2x+3)-4\) | |
| 450. |
Find the General Solution of the given differential equation.\((8x+7)\frac{dy}{dx}+2y=x\) |
| A. | \(c_1(\frac{1}{(8x+7)})^\frac{1}{4}+\frac{(8x+7)}{40}-\frac{5}{16}\) |
| B. | \(c_1(\frac{1}{(8x+7)})^\frac{1}{4}+\frac{(8x+7)}{80}-\frac{7}{8}\) |
| C. | \(c_1(\frac{1}{(8x+7)})^\frac{1}{4}+\frac{(8x+7)}{40}-\frac{7}{16}\) |
| D. | \(c_1(\frac{1}{(8x+7)})^\frac{1}{4}+\frac{(8x+7)}{80}-\frac{7}{16}\) |
| Answer» E. | |