Placement Papers for All Companies

3i infotech
Abacus Infotech
Abatix
Abaxis
ABB
ACC Limited
Accel Frontline
Accenture
Aditi Technologies
Adobe System
ADP
Agilysys
AgreeYa
AIG
AirNet
Alanco Technologies
Alle Technologies
Allfon
Alter Systems
Amazon
AMDL
Amdocs
AMI
Amiti Software Technologies
ANZ
Apple
Applied Materials
Apps Associates
Aricent
ASDC
Ashok Leyland Ltd
Asian Paints
Aspire System
AT & T
Atlas Copco
Atos Origin
AXA Technology Services
Axes Technology
Bain
Bajaj
Bayer
Bharti Airtel Ltd
Bhawan Cybertek
Birlasoft
Blue Star Infotech
BMC
BOB
Brakes India
C-DOT
CA Technologies
Cadence
Calsoft
Canarys
Capgemini
Caterpillar
Celstream
CGI Group
Changepond Technologies
Cimtrix Systems
Cisco system
Citicorp Overseas Software Ltd
ClinTech
CMC Limited
CMS
Cognizant
Compaq
Consagous Technologies
Convergys
CORDYS
CRISIL
Crompton Greaves
CSC
CSFB
CtrlS Datacenters Ltd
Cummins
Cyient
Daffodil
Daimler
Dell
Deloitte
Delphi-TVS
Dharma Systems
Directi
DSRC
Eicher
ELGI
ELICO
EMC Corporation
Emphasis
Ericsson
Ernst & Young
ESKO
Essar
Facebook
Fanuc Corporation
Fidelity
Flextronics
Flipkart
Freescale
Fujitsu
Gajshield
GE
Genpact India
Geodesic
Geometric Limited
GlobalEdge
GlobalLogic
GMR Group
Godrej Infotech
Google
Grapecity
Harita - TVS
HCL
HCL Technologies
Headstrong
Healthasyst
HEC Ltd
Hexaware
HFCL
Holool
Honeywell
HP
HTC Global Services
Huawei
Hughes
Hyundai
IBM
IBS Software Services
IGate
Ikanos
IKOS
Impetus
iNautix
Indecomm
IndiaBulls Power Limited
Inductis-EXL
Industrial Alliance
Infineon
Infogain
Infosys
Intec
Integra
Intel
Intergraph
ITC Infotech
Jindal Steel and Power Limited
KPIT
L & T
L & T Infotech
LG Soft
Linde India Ltd
LnT Emsys
LnT-ECC
Lucas - TVS
Mahindra Engineering Services Ltd
Mahindra Ltd
Maruti
Matrix
Maveric Systems
McAfee
Microland
Microsoft
Mindtree
Miraclesoft
MKCL
Motorola
Mu-Sigma
Nagarro
NASSCOM
NCR Corporation
Ness Technologies
Neudesic
NIIT Technologies
Novell
Nvidia
Oracle
Persistent
Philips
Planetasia
Polaris
Poornam Info Vision
PSI Data Systems Limited
Quest-Global
Quinnox
R Systems
Redpine
Reliance Energy
Robert Bosch
RS Software
Samsung
SAP labs India
Sapient
Sasken Communications
Schneider India
Serco
Siemens
Sierra Atlantic
SkyTECH
Soliton
Sonata Software
Sony India
SQL Star
Steria
Subex Limited
Sutherland Global Services
Syntel
Talisma
Tata motors
Tata technologies
Tata-ELXSI
TCE
TCS
Tech Mahindra
Temenos
Tesco
Texas Instruments
Thermax
ThoughtWorks
Torry Harris
Triad
Trianz
Trilogy
TVS Motor
Unisys
UnitedHealth Group
UST Global
UTC Aerospace System
Valuelabs
Vedanta
Verifone
Verizon
Virtusa
Vision Infotech
Vizual
VMware
Wipro
Yahoo
YASH Technologies
Zenith
Zensar Technologies
ZTE

Quest-Global Latest Technical Questions

Posted on :01-04-2016
Q1. Shot-peening is a process used for introducing a 

a. compressive surface layer
b. Use a hardening coating to improve metal properties
c. Reduce metal surface imperfection by machining
d. Is the process of coating with a anti-corrosive paint

 
Q2. The Oil system in Turbofan engine has the following roles

a. It cools the bearing and spline
b. It lubricates bearings and spline
c. Both 1 and 2
d. None of these


Q3. Variable geometry inlet duct are used on supersonic aircrafts for

a. Slowing the airflow to subsonic speeds at the face of the compressor and increase static pressure
b .accelerating the airflow, to supersonic speeds, during cruising flisht
c. Increasing the airflow, at outlet end of compressor
d. None of these


Q4. What are the metal removal techniques

a. Ultra High Pressure jet Machining
b. Electro Discharge Machining
c. elecctro Chemical Machining

 
Q5. Why do we need to to do Inspection

1.To determine whether the component is serviceable
2.To restore Fit,Form and Function of the component
3.To determine whether the component is repairable

a.Option 1 and 2
b.Option 1 and 3
c.Option 2 and 3
d All the above


Q6. Full Authority Digital Engine Control (FADEC)system

a. Decrease the Fault detection capability of the engine
b. Has no effect on Fault detection capability of the engine
c. Increase the fault detection capability of the engine 
d. None of the above


Q7. The surge magic of Centrifugal compressor is----than that of an Axial compressor

a.More
b.Less
c.Equal
d.Not adequate


Q8. In normal flight conditions, an increase in aircraft speed

a. Cause the nose of the aircraft to drop
b. Cause the nose of the aircraft to lift
c. The nose remains in the same position
d. None of these


Q9. With increasing altitude pressure decrease and 

a.Temperature decreases at the same rate as pressure reduces
b.Temperature decreases but at a lower rate than
c. Temperature remains constant to 8000 ft
d. None of these


Q10. Longitudinal stability is given by 

a. The fin
b. the wing dihedral
c. the horizontal tail plane
d. None of the above


Q11. What are the types of rivets that are used in Aerospace Industry

a.Solid river
b.Hollow river
c.Blind river

a.Option 1 and 2
b.Option 1 and 3
c.Option 2 and 3
d. All the above


Q12. During a glide the following forces act on an aircraft

a.lift,weight,thrust
b.Lift.drag,weight
c.Lift and weight only
d.None of the these
 
 
Q13. Which of the following properties makes titanium ideal for fan baldes

a. It is very light
b. It is very leap
c. It is silver coloured
d. all the above


Q14. What are the metal joining techniques

a. Welding
b. Brazing
c. Thermal spray Technique
d. Mechanical Fastner

a. Option 1,2 and 3
b. Option 2,3 and 4
c. Option 1,2 and 4
d. All the above


Q15. The Thermal Expansion of the Turbine casting is controlled throughout the cycle to

a. Maintain optimum clearance between Blade tip and case
b. To relieve the stresses developed in the casing
c. To support Engine Health Monitoring
d. To reduce Turbine speed


Q16. The component used for transferring axial thrust form a rotating component to a static component is

a. Roller Bearing
b.Thrust Bearing
c. Ball Bearing
d. Both 2 and 3 above


Q17. The boundary layer is 

a. Thicker at the leading edge
b. Thickest at the trailing edge
c. Constant thickness from leading to trailing edges
d. None of the above


Q16. Additional thrust is required for

a. Landing
b. Acceleration and climb
c. Decelerating aircraft
d. Cruise

 
Q18. With increase in pressure ration the specific fuel consumption

a.Increase
b.Decrease
c.remains constant
d.None of the above


Q19. An aircraft which is longitudinally stable, will tend to return to level flight after a movement about which axis

a.Pitch
b.Roll
c.Yaw
d.All the above


Q20. To ensure component integrity,types of Inspection Techniques used is

a.Visual inspection
b.Dimensional inspection
c. Non destructive Inspection
d. All the of the above


Q21. Rotating stall,surge and flutter can be overcome by the 

a. Variable stater Vanes
b. Introducing inter-stage bleed
c. Both the above
d. None of the above


Q22. Radiographic examination is performed

1.To identify the cracks
2.Ti identify internal defects  component
3.To identify the defects in magnetic material

a.Option 1 and 2
b.Option 1 and 3
c.Option 2 and 3
d. all the above


Q23. Specific Fuel consumption (SFC) is ratio of

a. Fuel Flow rate/Thrust
b.Thrust/Fuel/Flow rate
c.Thrust/Air mass flow rate
d. None of the above
 

  
   






FreshersLive - No.1 Job site in India. Here you can find latest 2016 government as well as private job recruitment notifications for different posts vacancies in India. Get top company jobs for both fresher and experienced. Job Seekers can get useful interview tips, resume services & interview Question and answer. Practice online test free which is helpful for interview preparation. Register with us to get latest employment news/rojgar samachar notifications. Also get latest free govt and other sarkari naukri job alerts daily through E-mail.

closepop
closepop