Dr. Asha Crasta

Designation: 
Associate Professor
Department: 
Maths

Qualification:  MSc, M.Phil, Ph.D

Experience: 11 Years

Dr. Asha Crasta has completed her Phd from Jain University , Bengaluru under the topic 'Estimation of stability derivatives for wedges and wings in supersonic and Hypersonic flow' and received the Gold Medal for the Best Phd Student for the academic year 2014-2015.

Dr. Asha Crasta has done her MSc from Mangalore University and her M. Phil from VMU, Salem . She was also awarded ' Best Presentation Award’ for the presentation at the Research Retreat held at Jain university Bangalore on 18-19 at August 2012.

Presentations

[1] Presented a paper entitled ' Oscillating supersonic delta wings with curved leading edges' in the 22nd international conference of Jangjeon mathematical society held on August 13-15, 2009 at Adichunchanagiri Institute of Technology, Chickmagalore.
[2] Presented a paper entitled ' Estimation of stability derivatives of a delta wing in Hypersonic flow' in the 22nd international conference of Jangjeon mathematical society held on August 13-15, 2009 at Adichunchanagiri Institute of Technology, Chickmagalore.
[3] Presented a paper on ' Estimation of stability derivatives of a Oscillating delta wing in Supersonic flow' in the 10th Asian symposium on Visualization organised by the school of Mechanical engineering, SRM university, India and Asian society for visualization between 1-5th march 2010.
[4] Presented a paper 'Estimation of stability derivatives of oscillating delta wings in hypersonic flow with curved leading edges at National Conference on 'Modern trends in science and technology, MTST- 11 held on October 14th and 15th 2011 at Dr. M.V.Shetty Institute of technology,Moodabidri.
[5] Presented a paper estimation of stability derivatives in pitch and roll of a delta wing at Research retreat organised by Jain University , Bangalore on 18-19 August 2012.

 
 
 
1. Asha Crasta and S. A. Khan, “High Incidence Supersonic similitude for Planar wedge”, International Journal of Engineering research and Applications, Vol. 2, Issue 5, September-October 2012, pp. 468-471.
2. Khan S. A. and Asha Crasta, “Oscillating Supersonic delta wings with curved leading edges”,
Advanced Studies in Contemporary mathematics, Vol. 20 (2010), No.3, pp. 359-372.
3. Asha Crasta and S. A. Khan, “Estimation of Stability derivatives of an Oscillating Hypersonic delta wings with curved leading edges”,IJMET, Vol.3, Issue 3, December 2012, pp. 483-492.
4. Asha Crasta, S. A. Khan , “ Determination of Surface Pressure of an axisymmetric ogive in Hypersonic Flow” in Mathematical sciences International Research Journal, Vol. 2, Issue2,August 2013,pp.333-335,ISSN:2278-8697.
5. Asha Crasta and S.A. Khan, 2014, ‘Estimation of Stability Derivatives for a Planar Wedge in the Newtonian Limit’, IOSR Journal of Mathematics, Volume10, Issue 2 Version I, March-April, pp. 01-06.
6. Asha Crasta and S. A. Khan, 2014, ‘Effect of Mach number on Stiffness and Damping Derivatives for Oscillating Hypersonic Non-Planar Wedge’, IOSR Journal of Mechanical and Civil Engineering ,Volume 11, Issue 2 Ver. VIII (Mar- Apr.), pp. 04-11.
7. Asha Crasta and S.A. Khan, 2014, ‘Effect of Angle of Incidence on Stiffness and Damping derivatives for Oscillating Hypersonic Non-planar Wedge’, International Journal for Research in Applied Science and Engineering Technology, Vol. 2, Issue IV, April 2014, pp. 229-242.
8. Asha Crasta and S. A. Khan, 2014, ‘Supersonic Similitude for Oscillating Non-Planar wedge’, IOSR Journal of Mathematics,Volume10, Issue 2 Ver.VI ,Mar-Apr 2014, pp.15-24.
9. Asha Crasta, M. A. Baig, S. A. Khan , 2012, ‘Estimation of Stability derivatives of a Delta wing in Hypersonic flow’, International Journal of Emerging trends in Engineering and Developments , Vol. 6, Issue2, Sep., pp. 505-516.
10. Asha Crasta and Khan S. A, 2012, ‘Oscillating Supersonic delta wing with Straight Leading Edges’, International Journal of Computational Engineering Research, Vol. 2, Issue 5, September, pp. 1226-1233.
11. Asha Crasta and Khan S. A., 2014, ‘Stability derivatives of a Delta Wing with Straight leading edge in the Newtonian Limit’, International Journal of Engineering research and Applications, Vol. 4, Issue 3, Version 2, March, pp. 32-38.
12. Asha Crasta and S. A. Khan, 2013, ‘Stability Derivatives in the Newtonian Limit’, International Journal of Advanced Research in Engineering and Technology, Volume 4, Issue 7, Nov-Dec., pp. 276-289.
13. Asha Crasta, S. A. Khan , 2014, ‘Effect of angle of incidence on Roll damping derivative of a delta Wing’, International Journal of Emerging trends in Engineering and Developments Vol. 2, Issue4, March 2014, pp. 343-356.
14. Asha Crasta and S.A. Khan, 2014, ‘Effect of Angle of Incidence on Stability derivatives of a wing’, International Journal for Research in Applied Science and Engineering Technology, Vol. 2, Issue V, May, pp. 411-422.
15. Asha Crasta and S. A. Khan, 2014 ,’Effect of Angle of attack on Stability derivatives of a Delta wing with Straight leading edge in Supersonic Flow’,International Journal of Mathematics,Vol.10,issue5,Sep-oct 2014. Pp. 01-08.
16. Asha Crasta and S. A. Khan, 2014, ‘Hypersonic similitude for planar wedges’, International Journal of Advanced Research in Engineering and Technology, Volume 5, Issue 2, Feb., pp. 16-31.
17. Asha Crasta, S. A. Khan , 2014, ‘Effect of sweep angle on Roll damping derivative of a delta Wing’, International Journal of Emerging trends in Engineering and Developments Vol15, Issue4, Aug-Sep, pp. 45-55.
18. Asha Crasta and S. A. Khan, 2014 ,’Effect of Angle of attack on Stability derivatives of a Delta wing in Hypersonic flow with Straight leading edge’,International Journal of Mechanical and civil engineering,Vol.11,issue5,Sep-oct (ver.2). Pp. 21-29.
19. Asha Crasta and S.A.Khan 2014,” Effect of sweep angle on rolling moment derivative of an oscillating supersonic/hypersonic delta wing”, International journal of modern Engg. Research, Vol.4, issue 10,ver3, pp.15-22.
20. Asha Crasta and S. A. Khan 2015, “Effect of Angle of attack on Stiffness derivative of an oscillating supersonic delta wing with curved leading edges” IOSR-JMCE issue1, Volume12, December,pp12-25.
21. Asha Crasta and S. A. Khan, “Effect of Angle of attack on Damping derivative of a delta wing with full sine curved leading edges” IJETED Journal issue5, Volume1, December- January 2015.
22. Asha Crasta and S. A. Khan,2015 “Estimation of Damping derivative of a delta wing with half sine curved leading edges” IOSR Journal of Mechanical and civil engineering, Vol.12, issue1,February ,pp40-44.
23. Asha Crasta and S. A. Khan 2015, “Estimation of Damping derivative in pitch of a Supersonic delta wing with curved leading edges” IOSR Journal of Journal of Mathematics , Vol. 11,issue 1, Jan-feb ,pp.07-15.

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