| osCIILATING SUPERsoNIC DELA WINGs. w CURVED LEADING EDGES SA Khan, A Crasta | 38 | 2010 |
| Oscillating Supersonic delta wing with Straight Leading Edges A Crasta, SA Khan International Journal of Computational Engineering Research 2 (5), 1226-1233, 2012 | 37 | 2012 |
| High incidence supersonic similitude for planar wedge A Crasta, SA Khan International Journal of Engineering research and Applications 2 (5), 468-471, 2012 | 32 | 2012 |
| Effect of Angle of Incidence on Stability derivatives of a wing A Crasta, SA Khan IET Digital Library, 2013 | 29 | 2013 |
| Estimation of Stability derivatives of a Delta wing in Hypersonic flow A Crasta, MA Baig, SA Khan International Journal of Emerging trends in Engineering and Developments 6 …, 2012 | 28 | 2012 |
| Hypersonic similitude for planar wedges A Crasta, SA Khan International Journal of Advanced Research in Engineering and Technology 5 …, 2014 | 27 | 2014 |
| Stability Derivatives in the Newtonian Limit A Crasta, SA Khan International Journal of Advanced Research in Engineering and Technology 4 …, 2013 | 25 | 2013 |
| Effect of angle of incidenceon roll damping derivative of a delta wing A Crasta, SA Khan International Journal of Emerging Trends in Engineering and Development 2 …, 2014 | 23 | 2014 |
| Supersonic Similitude for Oscillating Non-Planar wedge A Crasta, SA Khan IOSR Journal of Mathematics 10 (2), 15-24, 2014 | 21 | 2014 |
| Effect of Mach number on Stiffness and Damping Derivatives for Oscillating Hypersonic Non-Planar Wedge A Crasta, SA Khan IOSR Journal of Mechanical and Civil Engineering 11 (2), 04-11, 2014 | 20 | 2014 |
| „Stability derivatives of a Delta Wing with Straight leading edge in the Newtonian Limit‟ A Crasta, SA Khan International Journal of Engineering research and Applications 4 (3), 32-38, 2014 | 19 | 2014 |
| Effect of Angle of Incidence on Stiffness and Damping derivatives for Oscillating Hypersonic Non-planar Wedge A Crasta, SA Khan International Journal for Research in Applied Science and Engineering …, 2014 | 19 | 2014 |
| Estimation of Stability Derivatives for a Planar Wedge in the Newtonian Limit A Crasta, SA Khan IOSR Journal of Mathematics 10 (2), 01-06, 2014 | 19 | 2014 |
| Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow A Crasta, S Pavitra, SA Khan International Journal of Energy, Environment and Economics 24 (1), 67-73, 2016 | 17 | 2016 |
| Estimation of Stability derivatives of an Oscillating Hypersonic delta wings with curved leading edges A Crasta, SA Khan International Journal of Mechanical Engineering & Technology 3 (3), 483-492, 2012 | 17 | 2012 |
| „Effect of sweep angle on Roll damping derivative of a Delta Wing‟ A Crasta, SA Khan International Journal of Emerging trends in Engineering and Developments 5 …, 2014 | 15 | 2014 |
| Effect of Angle of attack on Stiffness derivative of an oscillating supersonic delta wing with curved leading edges A Crasta, SA Khan IOSR-JMCE issue1, Volume12, December, pp12-25, 2015 | 14 | 2015 |
| Effect of Angle of attack on Stability derivatives of a Delta wing with Straight leading edge in Supersonic Flow‟ A Crasta, SA Khan International Journal of Mathematics 10 (5), 01-08, 2014 | 13 | 2014 |
| Effect of Angle of attack on Stability Derivatives of a Delta wing in Hypersonic Flow with Straight leading edge‟ A Crasta, SA Khan International Journal of Mechanical and civil engineering 11 (5), 21-29, 2014 | 12 | 2014 |
| Estimation of Stability Derivatives in Newtonian Limit for Oscillating Cone A Shabana, RS Monis, A Crasta, SA Khan IOP Conference Series: Materials Science and Engineering 370 (1), 012061, 2018 | 11 | 2018 |
