Dr. Asha Crasta

Designation: 
Associate Professor
Department: 
Maths
Qualification: M.Sc, M.Phil, Ph.D
Experience: 13 Years (Teaching)

Dr. Asha Crasta has completed her Ph.d 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.She has done her M.Sc from Mangalore University and 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 18th-19th of August 2012

 
 

Research Interest

Aerodynamics, Fluid dynamics, Numerical analysis, Differential Calculus, linear programming, Graph theory, Number theory, Discrete Mathematical structures, operation research and statistics

International Conferences & Journals

  • 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

  • Khan S. A. and Asha Crasta, “Oscillating Supersonic delta wings with curved leading edges”in Advanced Studies in Contemporary mathematics, Vol. 20 (2010), No.3, pp. 359-372.

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • Asha Crasta and S.A.Khan 2015,”Effect of Aspect ratio with angle of attack of an oscillating Hypersonic delta wing with Straight Leading edges”, Mathematical Sciences International research Journal” ,volume 4 , issue2, pp.28-33., ISSN2278-8697

  • Asha Crasta and S.A. Khan,2016,”Effect of Aspect ratio with roll moment derivative of a delta wing in supersonic flow”, International Journal of Advances in Engineering Research, (IJAER) 2016, Vol. No. 12, Issue No. I, July,pp.10-15, e-ISSN: 2231-5152, p-ISSN: 2454-1796

  • Asha Crasta , Pavitra S, S.A. Khan 2016,” Estimation Of Surface Pressure Distribution On A Delta Wing With Curved Leading Edges In Hypersonic/Supersonic Flow” , International journal of energy ,environment and Economics,Nova Science publishers inc,Vol 24, pp.67-73

  • Pavitra S, Lavanya S, S.A. Khan, Asha Crasta 2016,” Estimation of Aerodynamic derivatives in pitch of a wedge in Hypersonic flow”, Indian Journal of Science and Technology. ,pp.1-4

 

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