Friday, April 25, 2014

SAEX1015(2010) , Aircraft Stability and Control 2013 Question Paper, B.E Aeronautical Engineering, Sathyabama University

Sathyabama University Question Papers for latest year 2013 have been illustrated below. Have a look at the following question paper which belongs to B.E Aeronautical Engineering. Get this Aircraft Stability and Control 2013 Question Paper.

SATHYABAMA UNIVERSITY
(Established under section 3 of UGC Act,1956)
Course & Branch : B.E - AERO
Title of the Paper : Aircraft Stability and Control
Max. Marks: 80
Sub. Code : SAEX1015(2010)
Time : 3 Hours
Date : 09/04/2013
Session : FN

PART - A (10 x 2 = 20)

Answer ALL the Questions

1. What is the effect of downwash at the tail?

2. Define – Elevator power. Write down its expression.

3. Write the conditions for longitudinal static stability.

4. Mention the methods to reduce the stick force gradient.

5. Define – Dihedral effect. What is positive dihedral?

6. Define - Roll Control Power.

7. What is Static Margin? What is its importance in the Airplane

8. What is Routh’s criterion for stability?

9. What is Feed Back control?

10. Mention any four essential advantages of Digital control system.

Look on the images below to read Part-B.

Duraimani

B.E Civil Engineer Graduated from Government College of Engineering Tirunelveli in the year 2016. She has developed this website for the welfare of students community not only for students under Anna University Chennai, but for all universities located in India. That's why her website is named as www.IndianUniversityQuestionPapers.com . If you don't find any study materials that you are looking for, you may intimate her through contact page of this website to know her so that it will be useful for providing them as early as possible. You can also share your own study materials and it can be published in this website after verification and reviewing. Thank you!