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Title: Elastic Quotas
Page Link: Elastic Quotas -
Posted By: computer science crazy
Created at: Tuesday 23rd of September 2008 03:27:03 AM
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Definition
Despite seemingly endless increases in the amount of storage and ever decreasing costs of hardware, managing storage is still expensive. Additionally, users continue to fill increasingly larger disks, worsened by the proliferation of large multimedia files and high-speed broadband networks. Storage requirements are continuing to grow at a rate of 50% a year. Worse, existing hard disk technology is reaching physical limitations, making it harder and costlier to meet growing user demands . Storage management costs have remained a sign ....etc

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Title: f 14 variable geometry wing advantages
Page Link: f 14 variable geometry wing advantages -
Posted By:
Created at: Saturday 26th of October 2013 09:04:49 PM
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Title: inflatable wing aircraft full report
Page Link: inflatable wing aircraft full report -
Posted By: project report tiger
Created at: Tuesday 16th of February 2010 12:09:27 AM
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Advantages of inflatable wings


High aspect ratio
High durability
We can change the value of CL
Can be packed and deployed numerous times
Wing can recover shape in flight even if the load limit is exceeded
Impact absorption and impact resiliency


Applications

Military applications
1.border patrol
2. surveillance and inspection.
Commercial applications
1. airborne observation of crops
2. inspection of pipelines and power lines.
3.mapping of particular area
Space research
....etc

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Title: The Impact of Active Aeroelastic Wing Technology on Conceptual Aircraft Design
Page Link: The Impact of Active Aeroelastic Wing Technology on Conceptual Aircraft Design -
Posted By: seminar class
Created at: Saturday 07th of May 2011 06:28:24 PM
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Abstract
Active Aeroelastic Wing (AAW) Technologyrepresents a new design approach for aircraft wingstructures. The technology uses static aeroelasticdeformations as a net benefit during maneuvering.AAW is currently being matured through a flightresearch program1; however, transition of thetechnology to future systems will require educatingdesigners in multiple disciplines of this new designapproach. In order to realize the full benefits of AAW,aeroelastic effects will need to be accounted for fromthe beginning of the design process. Co ....etc

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Title: ULTRA SONIC TECHNIQUES FOR THE DETECTION OF HIDDEN CORROSION IN AIR CRAFT WING SKIN
Page Link: ULTRA SONIC TECHNIQUES FOR THE DETECTION OF HIDDEN CORROSION IN AIR CRAFT WING SKIN -
Posted By: seminar projects crazy
Created at: Saturday 31st of January 2009 02:42:47 AM
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Detection of corrosion damage in aircraft wing skin structures is an ongoing NDT challenge. Ultrasonic methods are known and well-accepted techniques, which are relatively simple to carry out in terms of setup, probes and instrumentation and operator training. However, with conventional inspection from the top surface using a transducer at normal incidence (0o to the normal to the surface) producing a visual picture in the form of a C-scan, it is very tie consuming to point-by-point inspects large aircraft wing skin areas. In addition it is too ....etc

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Title: Flutter Characteristics of an Over-the-Wing Engine Mount Business-Jet Configuration
Page Link: Flutter Characteristics of an Over-the-Wing Engine Mount Business-Jet Configuration -
Posted By: seminar class
Created at: Wednesday 04th of May 2011 06:20:14 PM
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Abstract
Mounting engines on the wing causes complex wing
flutter characteristics. The location of the engine mass
and the stiffness of the pylon relative to the wing are
important in preventing hazardous wing flutter. In
addition, if the nacelles are installed over the wing,
aerodynamic interference between the wing and the
nacelle may cause unfavorable flutter characteristics, in
particular, at transonic speeds. The flutter
characteristics of an over-the-wing engine mount
configuration obtained from theoretical analyses and
....etc

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Title: ppt for wing fabrication of aircraft
Page Link: ppt for wing fabrication of aircraft -
Posted By:
Created at: Wednesday 17th of July 2013 09:44:36 AM
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HI,
I am a student from malaysia, i am currently do a project about fabrication of aircraft, i think this will be helpful to me. Hope that you can help me as soon as possible. ....etc

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Title: LINEMAN - PUBLIC WORKS -ELECTRICAL WING-kerala psc previous question paper
Page Link: LINEMAN - PUBLIC WORKS -ELECTRICAL WING-kerala psc previous question paper -
Posted By: anusree
Created at: Tuesday 25th of April 2017 01:53:58 PM
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1.Which one of the following is used as a passive-component in electric circuits?
(A)Resistor(B)Transistor
(C )Tunnel diode(D)Vaccum triode

2.The length of a conductor is doubled, then its resistance will be :
(A)Became same(B)Became halfed
(C )Became doubled(D)Four times increased

3. The defects of a primary cell is :
(A)Sulfation and buckling (C ) Sulphation and local action
(B) Local action and polarization (D) Buckling and polarization

4. The insulator used to separate commutator segment is :
(A)Asbestos(B ....etc

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Title: LINEMAN - PUBLIC WORKS - ELECTRICAL WING-KERALA PSC PREVIOUS QUESTION PAPER
Page Link: LINEMAN - PUBLIC WORKS - ELECTRICAL WING-KERALA PSC PREVIOUS QUESTION PAPER -
Posted By: anusree
Created at: Wednesday 12th of April 2017 05:31:33 PM
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1.The unit of solid angle is
A)radianB) steradian
C) degreeD) none of the above

2.What is the temperature co-efficient value of aluminum at 20° Celsius ?
A)40.3x10“*B) 40.3x1 O'3
C) 40.3x10_zD) 40.3 x10'5

3.How to increase the current range of a meter ?
A)A low resistance connected in series
B)A high resistance connected in series
C)A low resistance connected in parallel
D)A high resistance connected in parallel

4.One ampere-hour is equal to
A)36000 Coulombs C) 360 Coulombs
B) 3600 Coulombs D) 36 Coulo ....etc

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Title: ULTRASONIC TECHNIQUES FOR HIDDEN CORROSION DETECTION IN AIRCRAFT WING SKIN
Page Link: ULTRASONIC TECHNIQUES FOR HIDDEN CORROSION DETECTION IN AIRCRAFT WING SKIN -
Posted By: smart paper boy
Created at: Monday 29th of August 2011 05:08:35 PM
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INTRODUCTION
CAUSE OF CORROSION – MOISTURE, WATER, CRACKS
AREAS AFFECTED – SURFACE, LAP JOINTS, FASTENERS
3. NEED OF NDT
NON DESTRUCTIVE TESTS (NDT)
VISUAL INSPECTION
MAGNETIC PARTICLE TEST
LIQUID (DYE) PENITRATION TEST
X – RAY PENETRATION INSPECTION
EDDY CURRENT INSPECTION
ULTRASONIC INSPECTION
DEFECTS OF CONVENTIONAL SYSTEMS
INSPECTION FROM TOP NORMAL TO SURFACE
2. TIME CONSUMING FOR POINT TO POINT INSPECTION
3. INABILITY TO DETECT (a) DISBONDS IN MULTILAY ....etc

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