Items where Subject is "T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL780 Rockets"
Group by: Creator/Author | Item Type Number of items at this level: 32. AAhmed Ghazal, Belal and Ismail, Ahmad Faris (2011) The contribution of Hassan al-Rammah to gunpowder and rocket technology. In: Contributions of Early Muslim Scientists to Engineering Sciences and related studies. IIUM Press, Kuala Lumpur, pp. 36-40. ISBN 978-967-418-157-4 Ali Baig, Maughal Ahmed and Khan, Sher Afghan and Rathakrishnan, Ethirajan (2012) Active control of base pressure in suddenly expanded flow for area ratio 4.84. International Journal of Engineering Science and Technology (IJEST), 4 (5). pp. 1885-1895. ISSN 2278-9510 Asad Ullah, Mohammed and Bashir, Musavir and Janvekar, Ayub and Khan, Sher Afghan (2016) Active control of wall pressure flow field at low supersonic Mach numbers. IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE), 3. pp. 90-98. ISSN 2320-334x Ashfaq, Syed and Khan, Sher Afghan (2014) Influence of micro jets on wall pressure for area ratio 3.24. International Journal of Emerging Technology and Advanced Engineering (IJETAE), 4 (2). pp. 872-880. ISSN 2250-2459 Ashfaq, Syed and Khan, Sher Afghan (2014) Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25. International Journal of Engineering Science & Advanced Technology, 4 (1). pp. 49-60. ISSN 2250-3676 Azami, Muhammad Hanafi and Savill, Mark (2016) Comparative analysis of alternative fuels in detonation combustion. In: 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 25th-27th July 2016, Salt Lake City, Utah, US. BBaig, Maugal Ahmed Ali and Khan, Sher Afghan and Rathakrishnan, E. (2012) Experimental investigations on wall pressure in suddenly enlarged ducts at supersonic Mach number regimes. International Journal of Emerging Trends in Engineering and Development (IJETED), 6 (2). pp. 496-504. ISSN 2249-6149 Bashir, Musavir and Khan, Sher Afghan and Rajendran, Parvathy (2015) Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow. In: International Conference on Mechanical Engineering And Advanced Material (ICME-AM) 2015, 3rd-4th Dec. 2015, Kota Kinabalu, Sabah. CChaudhary, Zakir Ilahi and Shinde, V.B and Ashfaq, Syed and Khan, Sher Afghan (2015) Effect of level of expansion and inertia level in a suddenly expanded flow. In: International Conference on Mechanical Engineering & Advanced Material (ICME-AM2015), 3rd-4th Dec. 2015, Kota Kinabalu, Sabah. Chaudhary, Zakir Ilahi and Shinde, Vilas B. and Khan, Sher Afghan (2018) Investigation of base flow for an axisymmetric suddenly expanded nozzle with micro JET. International Journal of Engineering & Technology, 7 (3.29 (Special issue 29)). pp. 236-242. ISSN 2227-524X Chaudhary, Zakir Ilahi and Vilas B., Shinde and Khan, Sher Afghan (2015) Effectiveness of micro-jets at different level of expansion. IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE, 12 (4). pp. 29-34. ISSN 2278-3008 (O), 2319-7676 (P) 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 (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 (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 (2013) Stabilty derivatives in the newtonian limit. International Journal of Advanced Research in Engineering & Technology (IJARET), 4 (7). pp. 276-289. ISSN 0976-6480 KKhan, Sher Afghan and Abid, Abdul and Baig, Maugal Ahmed Ali (2018) CFD analysis of CD nozzle and effect of nozzle pressure ratio on pressure and velocity for suddenly expanded flows. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD), 8 (3). pp. 1147-1157. ISSN 2249-6890 Khan, Sher Afghan and Rathakrishnan, E. (2006) Control of suddenly expanded flow. Aircraft Engineering and Aerospace Technology, 78 (4). pp. 293-309. ISSN 0002-2667 Khan, Sher Afghan and Rathakrishnan, E. (2006) Nozzle expansion level effect on a suddenly expanded flow. International Journal of Turbo & Jet-Engines, 23 (4). pp. 233-257. ISSN 0334-0082 Khan, Sher Afghan (2015) Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow. In: International Conference on Mechanical Engineering And Advanced Material (ICME-AM) 2015, 3rd-4th Dec. 2015, Kota Kinabalu, Sabah. Khan, Sher Afghan and G M, Fharukh Ahmed (2016) Experimental study of suddenly expanded flow from correctly expanded nozzles. In: 2nd International Conference on Design, Analysis, Manufacturing & Simulation, 7th-8th April 2016, Chennai, India. OOng, Jiunn Chit and Omar, Ashraf Ali E. and Asrar, Waqar (2013) A BGK-based two-equation turbulence model algorithm for solving compressible navier-stokes equations. CFD Letters, 6 (2). pp. 46-61. ISSN 2180-1363 PPathan, Khizar Ahmed and Dabeer, Prakash S and Khan, Sher Afghan (2019) Influence of expansion level on base pressure and reattachment length. CFD Letters, 11 (5). pp. 22-36. ISSN 2180-1363 Pathan, Khizer Ahmed and Dabeer, Prakash S and Khan, Sher Afghan (2019) Effect of nozzle pressure ratio and control jets location to control base pressure in suddenly expanded flows. Journal of Applied Fluid Mechanics, 12 (4). pp. 1127-1135. ISSN 1735-3572 QQuadros, Jaimon Dennis and Khan, Sher Afghan and A. J., Antony (2018) Study of effect of flow parameters on base pressure in a suddenly expanded duct at supersonic mach number regimes using CFD and design of experiments. Journal of Applied Fluid Mechanics, 11 (2). pp. 483-496. ISSN 1735-3572 Quadros, Jaimon Dennis and Khan, Sher Afghan and Antony, A J (2018) Base pressure behaviour in a suddenly expanded duct at supersonic mach number regimes using Taguchi design of experiments. Mechanics and Mechanical Engineering, 22 (4). pp. 1077-1097. ISSN 1428-1511 Quadros, Jaimon Dennis and Khan, Sher Afghan and Antony, A J and S.Vas, Jolene (2016) Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for mach 3.0 using CFD. International Journal of Energy, Environment, and Economics, 24 (1). pp. 87-97. ISSN 1054-853X Quadros, Jaimon Dennis and Khan, Sher Afghan and A. J., Antony and Vas, Jolene S. (2016) Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD. In: International Conference on Energy Systems and Developments (ICESD2016), 19th-20th Feb. 2016, Pune, India. RRehman, Shafiqur and Khan, Sher Afghan (2008) Control of base pressure with micro jets:part-I. Aircraft Engineering and Aerospace Technology, 80 (2). pp. 158-164. ISSN 0002-2667 SSethuraman, Vigneshvaran and Thong, Kenny Tan Boon and Khan, Sher Afghan (2016) Effect of sudden expansion for varied area ratios at subsonic and sonic flow regimes. In: International Conference on Energy Systems and Developments (ICESD2016), 19th-20th Feb. 2016, Pune, India. 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 Syed, Syed Ashfaq and Khan, Sher Afgha (2015) Combined effect of relief and level of expansion in a suddenly expanded flow. IOSR Journal , 12 (5). pp. 52-59. ISSN e-ISSN: 2279-0837, p-ISSN: 2279-0845. ZZulkifli, Mohammad and Omar, Ashraf Ali and Asrar, Waqar (2014) Arbitrary Lagrangian-Eulerian Form of Flowfield Dependent Variation (ALE-FDV) Method for 3D Problems. In: 22nd Annual Conference of the CFD Society of Canada, 1-4 Jun 2014, Toronto Canada. (In Press) |