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Search: Posts Made By: Pradeep747
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8th May 2011, 07:14
Replies: 3,614
Views: 1,212,461
Posted By Pradeep747

Good News

Guys,Now exam is free of cost and cool off period is reduced to 3months.So all the best for all.Work hard.This is genuine opportunity we have got.So lets go get it...
21st Feb 2011, 14:06
Replies: 2,488
Views: 936,864
Posted By Pradeep747

Help Req

pressure req to compress the hydraulic fluid?
13th Jan 2011, 17:30
Replies: 2,488
Views: 936,864
Posted By Pradeep747

i would not send the email to anyone as the info...

i would not send the email to anyone as the info is not for us...imagine 5000 applicant sending email to HR...he will go mad.so its better not to mess things up...so we will do wat is asked from us...
13th Jan 2011, 16:08
Replies: 2,488
Views: 936,864
Posted By Pradeep747

Exams likely by Feb 27th.. info from ...

Exams likely by Feb 27th..

info from

http://igrua.gov.in/News/Jet%20Airways%20Selection.pdf
8th Dec 2010, 14:55
Replies: 3,614
Views: 1,212,461
Posted By Pradeep747

Thank u very much Euindkan..its so simple and i...

Thank u very much Euindkan..its so simple and i was taking it big and faltered.

@flyrock& Dynamite- Expect these kind of question and these are the question which is going to make u clear the exam...
8th Dec 2010, 11:05
Replies: 3,614
Views: 1,212,461
Posted By Pradeep747

Help Needed

Q-An aeroplane performs a steady horizontal turn with a TAS of 200 kt. The turn radius is 2000 m. The load factor (n) is approximately:
a)1.1
b)1.4
c)1.8
d)2.0

It says answer is 1.1
8th Dec 2010, 10:35
Replies: 3,614
Views: 1,212,461
Posted By Pradeep747

answer is No effect because camber of the...

answer is No effect because camber of the aerofoil produces constant pitch down moment independent of AOA
8th Dec 2010, 10:12
Replies: 3,614
Views: 1,212,461
Posted By Pradeep747

@kinko-not all r from oxford 4. In what way...

@kinko-not all r from oxford

4. In what way is the longitudinal stability affected by the degree of positive camber of the aerofoil?
7th Dec 2010, 17:24
Replies: 3,614
Views: 1,212,461
Posted By Pradeep747

Leading edge flaps Increases critical AOA and...

Leading edge flaps Increases critical AOA and trailing edge reduces critical AOA
7th Dec 2010, 15:31
Replies: 3,614
Views: 1,212,461
Posted By Pradeep747

@LOFT-U r right again.Guys every body post some...

@LOFT-U r right again.Guys every body post some question also...
Q3.What are frangible objects?
7th Dec 2010, 15:29
Replies: 3,614
Views: 1,212,461
Posted By Pradeep747

I believe its 0.5Nm or 3% which ever is higher

I believe its 0.5Nm or 3% which ever is higher
7th Dec 2010, 14:48
Replies: 3,614
Views: 1,212,461
Posted By Pradeep747

Q2.De Compression Sickness is related with 1....

Q2.De Compression Sickness is related with
1. Henry's Law
2. Dalton Law
3. Boyle Law
4.Charles law
7th Dec 2010, 14:43
Replies: 3,614
Views: 1,212,461
Posted By Pradeep747

:Bingo!!!!!Cheers LOFT:D It will be highly...

:Bingo!!!!!Cheers LOFT:D
It will be highly appreciated if u can solve it here in details
7th Dec 2010, 11:48
Replies: 3,614
Views: 1,212,461
Posted By Pradeep747

Lets brush up our knowledge!!!

Q1.Mass-50000kg
L/D-10
Thrust-30000N/Engine
G-10m/s2
Find the climb gradient for 3 engine airplane?
9th Aug 2010, 16:25
Replies: 393
Views: 64,914
Posted By Pradeep747

Dear Abhi, I can understand your...

Dear Abhi,
I can understand your feelings and effort you have put in..i just want to tell you one things...Do your work with sincerity and do our best in all circumstances,leaving the...
3rd Apr 2010, 16:45
Replies: 106
Views: 32,924
Posted By Pradeep747

About The Test

Hi What do they test you on...share your experience with CAE selection process pl
Showing results 1 to 16 of 16


 
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