# Items where Subject is "T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL780 Rockets"

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**TL780 Rockets**(53)

- TL Motor vehicles. Aeronautics. Astronautics (53)

- T Technology (53)

**53**.

## A

Aabid, Abdul and Khan, Sher Afghan
(2020)
*Investigation of high-speed flow control from CD nozzle using design of experiments and CFD methods.*
Arabian Journal of Science and Engineering.
pp. 1-30.
ISSN 2193-567X
E-ISSN 2191-4281
(In Press)

Afifi, Azmil and Aabid, Abdul and Khan, Sher Afghan
(2020)
*Numerical investigation of splitter plate effect on the bluff body using finite volume method.*
Materials Today: Proceedings (10.1016/j.matpr.2020.05.559).
pp. 1-10.
ISSN 2214-7853
(In Press)

Afzal, Asif and Aabid, Abdul and Khan, Ambareen and Khan, Sher Afghan and Rajak, Upendra and Verma, Tikendra Nath and Kumar, Rahul
(2020)
*Response surface analysis, clustering, and random forest regression of pressure in suddenly expanded high-speed aerodynamic flows.*
Aerospace Science and Technology, 107.
pp. 1-30.
ISSN 1270-9638

Afzal, Asif and Khan, Sher Afghan and Islam, Md. Tariqul and Jilte, R. D. and Khan, Ambareen and Soudagar, Manzoore Elahi M
(2020)
*Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers.*
Physics of Fluids, 32 (9).
pp. 1-18.
ISSN 1070-6631
E-ISSN 1089-7666

Ahmed 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
E-ISSN 0975-5462

Ansari, Emad and Siddiqui, M. Umair and Khan, Sher Afghan and Akhtar, Mohammad Nishat and Ilmi, Abu Bakar
(2020)
*Numerical investigation of mathematical non-dimensional
constant representing smoothness in the Nusselt profile.*
CFD Letters, 12 (6).
pp. 16-27.
ISSN 2180-1363

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
E-ISSN 2278-1684

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 Faheem, Mohammed and Aabid, Abdul and Mokashi, Imran and Khan, Sher Afghan
(2019)
*Experimental research of wall pressure distribution and effect of micro jet at Mach 1.5.*
International Journal of Recent Technology and Engineering (IJRTE), 8 (2S3).
pp. 1000-1003.
E-ISSN 2277-3878

Azami, Muhammad Hanafi and Faheem, Mohammed and Aabid, Abdul and Mokashi, Imran and Khan, Sher Afghan
(2019)
*Inspection of supersonic flows in a CD nozzle using experimental method.*
International Journal of Recent Technology and Engineering (IJRTE), 8 (2S3).
pp. 996-999.
ISSN 2277-3878

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.

## B

Baig, 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 Choudhary, Zakir Ilahi and Shinde, V. S.
(2020)
*Wall Pressure Measurements Beneath the Supersonic Jets in
an Abruptly Augmented Nozzle.*
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 66 (2).
pp. 20-31.
ISSN 2289-7879

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.

## C

Chaudhary, 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

## G

G M, Fharukh and Khan, Sher Afghan
(2019)
*Control of nozzle flow using microjets at supersonic Mach Regime.*
International Journal of Engineering, 32 (7).
pp. 991-998.
ISSN 1025-2495
E-ISSN 1735-9244

G. M, Fharukh Ahmed and Khan, Sher Afghan
(2019)
*Role of active control in increasing base pressure at Sonic Mach Number.*
International Journal of Recent Technology and Engineering, 8 (2S3).
pp. 966-970.
E-ISSN 2277-3878

## K

Khan, Sher Afghan and Aabid, Abdul and Chaudhary, Zakir Ilahi
(2019)
*Influence of control mechanism on the flow field of duct at Mach 1.2 for area ratio 2.56.*
International Journal of Innovative Technology and Exploring Engineering (IJITEE), 8 (6S4).
pp. 1135-1138.
ISSN 2278-3075

Khan, 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
E-ISSN 2249-8001

Khan, Sher Afghan and Ahmad, Zaheer and Aabid, Abdul and Mokashi, Imran
(2019)
*Experimental research on flow development and control effectiveness in the duct at high speed.*
International Journal of Recent Technology and Engineering (IJRTE), 8 (2S8).
pp. 1763-1768.
E-ISSN 2277-3878

Khan, Sher Afghan and Bashir, Musavir and Baig, Maugal Ahmed Ali and Mehaboob Ali, Fharukh Ahmed Ghasi
(2020)
*Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics.*
CFD Letters, 12 (3).
pp. 1-10.
ISSN 2180-1363

Khan, Sher Afghan and Mokashi, Imran and Aabid, Abdul and Faheem, Mohammad
(2019)
*Experimental research on wall pressure distribution in C-D nozzle at Mach number 1.1 for area ratio 3.24.*
International Journal of Recent Technology and Engineering, 8 (2S3).
pp. 971-975.
E-ISSN 2277-3878

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
E-ISSN 2191-0332

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.

## O

Ong, 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

## P

Pathan, 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, Khizar Ahmed and Dabeer, Prakash S and Khan, Sher Afghan
(2020)
*An investigation of effect of control jets location and blowing pressure ratio to control base pressure in suddenly expanded flows.*
Journal of Thermal Engineering,, 6 (2 (Special Issue 11)).
pp. 15-23.
E-ISSN 2148-7847

Pathan, Khizar Ahmed and Syed, Ashfaq and Dabeer, Prakash S and Khan, Sher Afghan
(2019)
*Analysis of parameters affecting thrust and base pressure in
suddenly expanded flow from nozzle.*
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 64 (1).
pp. 1-18.
ISSN 2289-7879

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
E-ISSN 1735-3645

Pathan, Khizer Ahmed and Dabeer, Prakash S and Khan, Sher Afghan
(2020)
*Enlarge duct length optimization for suddenly expanded flows.*
Advances in Aircraft and Spacecraft Science, 7 (3).
pp. 203-214.
ISSN 2287-528X
E-ISSN 2287-5271

## Q

Quadros, 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
E-ISSN 1735-3645

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
E-ISSN 2354-0192

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 T., Prashanth
(2020)
*Experimental and numerical investigation of expansion corner effects on isolator performance.*
International Journal of Turbo & Jet Engines, Ahead of print.
pp. 1-8.
ISSN 0334-0082
E-ISSN 2191-0332
(In Press)

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.

## R

Rehman, 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

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

## S

Sethuraman, Vigneshvaran and Rajendaran, Parvathy and Khan, Sher Afghan
(2020)
*Base and wall pressure control using cavities and ribs in suddenly expanded flows -an overview.*
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 66 (1).
pp. 120-134.
ISSN 2289-7879

Sethuraman, Vigneshvaran and Rajendran, Parvathy and Khan, Sher Afghan
(2019)
*A cost-effective data acquisition instrumentation for
measurement of base pressure and wall pressure in suddenly expanded flow through ducts.*
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 60 (1).
pp. 112-123.
E-ISSN 2289-7879

Sethuraman, 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
E-ISSN 2278-1684

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.

## Z

Zulkifli, 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)