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Items where Author is "Crasta , Asha"

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Number of items: 24.

Article

Crasta, Asha and Shabana, Aysha and Monis, Renita and Khan, Sher Afghan (2016) Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow. IOSR Journal of Mechanical & Civil Engineering, 12 (6). pp. 97-104. ISSN 2320-334x

Shabana, Ayesha and Monis, Renita and Crasta, Asha and Khan, Sher Afghan (2016) Pressure and its derivative with respect to piston Mach number for an oscillating cone. IOSR journal of Mechanical and Civil Engineering ( IOSR-JMCE ), 18 (6). pp. 74-78. ISSN 2320-334X

Monis, Renita Sharon and Shabana, Ayesha and Crasta, Asha and Khan, Sher Afghan (2016) Supersonic flow analysis and evaluation of damping derivative. IOSR Journal of Mechanical & Civil Engineering (IOSR-JMCE), 18 (6). pp. 29-36. ISSN 2320-334x

Shanbhag, Pavithra and Lavanya, S and Khan, Sher Afghan and Crasta, Asha (2016) Estimation of aerodynamic derivatives in pitch of a wedge in hypersonic flow. Indian Journal of Science and Technology, 9 (34). pp. 1-4. ISSN 0974-6846

Crasta, Asha and Khan, Sher Afghan (2016) Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow. International Journal of Advances in Engineering Research (IJAER), 12 (1). pp. 10-15. ISSN 2454-1796

Crasta, Asha and Pavithra, S and Khan, Sher Afghan (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, 24 (1). pp. 67-73. ISSN 1054-853X

Crasta, Asha and Khan, Sher Afghan (2015) Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge. International Journal of Emerging trends in Engineering and Development (IJETED), 5 (1). pp. 237-245. ISSN 2249-6149

Crasta, Asha and Khan, Sher Afghan (2015) Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges. Mathematical Sciences International Research Journal, 4 (2). pp. 28-33. ISSN 2278-8697

Crasta, Asha and Khan, Sher Afghan (2014) Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges. IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE), 11 (6vIII). pp. 12-25. ISSN 2320-334X

Crasta, Asha and Khan, Sher Afghan (2014) Effect of angle of incidence on stability derivatives of a wing. International Journal for Research in Applied Science and Engineering Technology (IJRASET), 2 (V). pp. 411-422. ISSN 2321-9653

Crasta, Asha and Khan, Sher Afghan (2014) Effect of angle of incidence on roll damping derivatives of a delta wing. International Journal of Emerging trends in Engineering and Development (IJETED), 4 (2). pp. 343-356. ISSN 2249-6149

Crasta, Asha and Khan, Sher Afghan (2014) Effect of mach number on stiffness and damping derivatives for oscillating hyersonic non-planar wedge. IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE), 11 (2vVIII). pp. 4-11. ISSN 2320-334X

Crasta, Asha and Khan, Sher Afghan (2014) Estimation of stability derivatives for a planar wedge in the newtonian limit. IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE, 10 (2 ). pp. 1-6. ISSN 2278-3008 (O), 2319-7676 (P)

Crasta, Asha and Khan, Sher Afghan (2014) Supersonic similitude for oscillating non-planar wedge. IOSR Journal of Mathematics (IOSR-JM), 10 (2vVI). pp. 15-24. ISSN 2319-7676

Crasta, Asha and Khan, Sher Afghan (2014) Hypersonic similitude for planar wedges. International Journal of Advanced Research in Engineering and Technology (IJARET), 5 (2). pp. 16-31. ISSN 0976-6480

Crasta, Asha and Khan, Sher Afghan (2013) Stabilty derivatives in the newtonian limit. International Journal of Advanced Research in Engineering & Technology (IJARET), 4 (7). pp. 276-289. ISSN 0976-6480

Crasta, Asha and Khan, Sher Afghan (2013) Stability derivatives of a delta wing with straight leading edge in the Newtonian limit. International Journal of Engineering Research and Application, 4 (2). pp. 1482-1488. ISSN 2248-9622

Crasta, Asha and Khan, Sher Afghan (2012) High incidence supersonic similitude for planar wedge. International Journal of Engineering Research and Application, 2 (5). pp. 468-471. ISSN 2248-9622

Crasta, Asha and Baig, Maugal Ahmed Ali and Khan, Sher Afghan (2012) Estimation of stability derivatives of a delta wing in hypersonic flow. International Journal of Emerging trends in Engineering and Development (IJETED), 6 (2). pp. 505-516. ISSN 2249-6149

Crasta, Asha and Khan, Sher Afghan (2012) Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges. International Journal of Mechanical Engineering & Technology, 3 (3). pp. 483-492. ISSN 0976-6359

Crasta, Asha and Khan, Sher Afghan (2012) Oscillating supersonic delta wing with straight leading edges. International Journal of Computational Engineering Research,, 2 (5). pp. 1226-1233. ISSN 2250-3005

Crasta, Asha and Khan, Sher Afghan (2012) Oscillating supersonic delta wings with straight leading edges. International Journal of Computational Engineering Research,, 2 (5). pp. 12028-12035. ISSN 2250-3005

Khan, Sher Afghan and Crasta , Asha (2010) Oscillating supersonic delta wings with curved leading edges. Advanced Studies in Contemporary Mathematics, 20 (3). pp. 359-372. ISSN 1229-3067

Conference or Workshop Item

Shanbhag, Pavitra and Lavanya , S and Khan, Sher Afghan and Crasta, Asha (2016) Estimation of aerodynamic derivatives in pitch of a wedge in hypersonic flow. In: 2nd International Conference on Design, Analysis, Manufacturing & Simulation, 7th-8th April 2016, Chennai, India. (Unpublished)

This list was generated on Sun Nov 19 16:40:49 2017 +08.