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Items where Author is "Crasta, Asha"

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Shabana, Ayesha and Bayar, Anitha Dayanand and Crasta, Asha and Khan, Sher Afghan and Baig, Maughal Ahmed Ali and Reddy, Voggu Kesava (2023) Evaluation of stability derivatives of an Ogive in a Newtonian limit. In: International Conference on Advances in Signal Processing Communications and Computational Intelligence, 23rd - 24th July 2021, Hyderabad, India.

Crasta, Asha and Khan, Sher Afghan and Baig, Maugal Ahmed Ali and Reddy, Chamakura Abhinav (2023) Stiffness derivative for a non-planar wedge in Newtonian limit. In: International Conference on Advances in Signal Processing Communications and Computational Intelligence, 23rd - 24th July 2021, Hyderabad, India.

Shamitha, A and Crasta, Asha and Khan, Sher Afghan (2023) Evaluation of derivative in damping in the Newtonian limit for non-planar wedge. Materials Today. pp. 1-3. ISSN 2214-7853 (In Press)

A., Shamitha and Crasta, Asha and Pathan, Khizer Ahmed and Khan, Sher Afghan (2023) Analytical and numerical simulation of surface pressure of an oscillating wedge at hypersonic Mach numbers and application of Taguchi's method. Journal of Advanced Research in Applied Sciences and Engineering Technology, 30 (1). pp. 15-30. ISSN 2462-1943

Shamitha, Shamitha and Crasta, Asha and Pathan, Khizar Ahmed and Khan, Sher Afghan (2023) Numerical simulation of surface pressure of a wedge at supersonic Mach numbers and application of design of experiments. Journal of Advanced Research in Applied Mechanics, 101 (1). pp. 1-18. E-ISSN 2289-7895

Shabana, Aysha and Crasta, Asha and Khan, Sher Afghan and Aabid, Abdul and Baig, Muneer (2022) Computation of stiffness and damping derivatives of an Ogive in a limiting case of mach number and specific heat ratio. Fluid Dynamics & Materials Processing, 23 (3). pp. 1-19. ISSN 1555-256X E-ISSN 1555-2578

Ayesha, Shabana and Crasta, Asha and Ridwan, R and Khan, Sher Afghan (2022) Computation of damping derivative of an Ogive at highspeed flow. Journal of Mechanical Engineering Research and Developments, 45 (2). pp. 151-165. ISSN 1024-1752

Renita, sharon Monis and Crasta, Asha and Khan, Sher Afghan and Parvathy, Rajendran and Erwin, Sulaeman (2022) Comparative study of quasi steady and unsteady damping derivatives for delta wings in hypersonic flow for half sine wave. Journal of Advanced Research in Fluid Mechanics and Thermal Science, 92 (1). pp. 1-8. ISSN 22897879 E-ISSN 2811-3950

Shabana, Aysha and Shamitha, A and Crasta, Asha and Khan, Sher Afghan (2021) Estimation of stiffness derivative for ogives at constant specific heat ratio γ = 1.666 at hypersonic mach numbers. Turkish Journal of Computer and Mathematics Education (TURCOMAT), 12 (10). pp. 316-325. E-ISSN 1309-4653

Renita, sharon Monis and Crasta, Asha and Khan, Sher Afghan (2020) Estımatıon of hypersonıc unsteady and qausı-steady dampıng derıvatıves for a delta wings at large incıdence. International Journal of Advanced Science and Technology, 29 (6). pp. 6844-6863. ISSN 2005-4238 E-ISSN 2207-6360

SHAMITHA, A and Crasta, Asha and Khan, Sher Afghan and VASAVI, P (2020) Computation of stability derivative for a wing for specific heat ratio= 1.66 for hypersonic flow. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD), 10 (special Issue). pp. 208-218. ISSN 2249–6890 E-ISSN 2249–8001

Renita, sharon Monis and Crasta, Asha and Khan, Sher Afghan (2020) Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number. Test Engineering & Management, 83 (2). pp. 13808-13819. ISSN 0193-4120

Shabana, Aysha and Monis, Renita Sharon and Crasta, Asha and Khan, Sher Afghan (2019) Estimation of stiffness derivative of an ogive for specific heat ratio 1.666. Test Engineering and Management, 81 (11-12). pp. 5091-5100. ISSN 0193-4120

Renita, sharon Monis and Crasta, Asha and Khan, Sher Afghan (2019) Estimation of damping derivatives for delta wings in hypersonic flow for straight leading edge. International Journal of Mechanical and Production Engineering Research and Development, 9 (5). pp. 255-264. ISSN 2249-6890 E-ISSN 2249-8001

Renita, sharon Monis and Crasta, Asha and Faheem, Mohammed and Khan, Sher Afghan (2019) Analysis of damping derivatives for delta wings in hypersonic flow for curved leading edges with full sine wave. International Journal of Engineering and Advanced Technology (IJEAT), 9 (1). pp. 5457-5466. ISSN 2249-8958

Shabana, Aysha and Monis, Renita Sharon and Crasta, Asha and Khan, Sher Afghan (2019) Damping derivative evaluation in pitch for an ogive at high mach numbers. International Journal of Innovative Technology and Exploring Engineering (IJITEE), 8 (12). pp. 1307-1317. E-ISSN 2278-3075

Monis, Renita Sharon and Shabana, Aysha and Crasta, Asha and Khan, Sher Afghan (2019) Effect of sweep angle and a half sine wave on roll damping derivative of a Delta Wing. International Journal of Recent Technology and Engineering, 8 (2S3). pp. 984-989. E-ISSN 2277-3878

Monis, Renita Sharon and Crasta, Asha and Khan, Sher Afghan (2019) An effect of sweep angle on roll damping derivative for a Delta wing with curved leading edges in unsteady flow. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD), 9 (2). pp. 361-373. ISSN 2249-6890 E-ISSN 2249-8001

Renita, Sharon Monis and Crasta, Asha and Khan, Sher Afghan (2019) Evaluation of stiffness derivative for a delta wing with straight leading edges in unsteady flow. International Journal of Engineering and Advanced Technology (IJEAT), 8 (3S). pp. 754-762. ISSN 2249 – 8958

Shabana, Ayesha and Renita, sharon Monis and Crasta, Asha and Khan, Sher Afghan (2018) The computation of stiffness derivative for an ogive in the hypersonic flow. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD), 8 (5). pp. 173-184. ISSN 2249-6890 E-ISSN 2249-8001

Shabana, Aysha and Monis, Renita Sharon and Crasta, Asha and Khan, Sher Afghan (2018) Effect of semi vertex angle on stability derivatives for an oscillating cone for constant value of specific heat ratio. International journal of Engineering & Technology, 7 (3.29). pp. 386-390. ISSN 2227-524X

Shabana, Aysha and Monis, Renita Sharon and Crasta, Asha and Khan, Sher Afghan (2018) Estimation of stability derivatives in newtonian limit for oscillating cone. In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017, 21-22 November 2017, Parkroyal HotelBatu Ferringhi, Penang; Malaysia.

Shabana, Aysha and Monis, Renita Sharon and Crasta, Asha and Khan, Sher Afghan (2018) Computation of stability derivatives of an oscillating cone for specific heat ratio = 1.66. In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017, 21 - 22 November 2017, Parkroyal HotelBatu Ferringhi, Penang.

Monis, Renita Sharon and Shabana, Ayesha and Crasta, Asha and Khan, Sher Afghan (2017) Computation of stiffness derivative for an unsteady delta wing with curved leading edges. International Journal of Recent Research Aspects .., 4 (4). pp. 69-72. ISSN 2349-7688

Shabana, Ayesha and Monis, Renita Sharon and Crasta, Asha and Khan, Sher Afghan (2017) Estimation of stability derivative of an oscillating cone in hypersonic flow. International Journal of Recent Research Aspectsh, 4 (4). pp. 46-52. ISSN 2349-7688

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 E-ISSN 2278-1684

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 E-ISSN 2278-1684

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 E-ISSN 2278-1684

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 E-ISSN 0974-5645

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 E-ISSN 2231-5152

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)

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 E-ISSN 2278-1684

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 E-ISSN 2278-1684

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 E-ISSN 2278-3008

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 E-ISSN 0976-6499

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

This list was generated on Fri Mar 29 19:25:35 2024 +08.