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

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**TL780 Rockets**(72)

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- T Technology (72)

**72**.

## 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)

Aabid, Abdul and Khan, Sher Afghan and Afzal, Asif and Baig, Muneer
(2021)
*Investigation of tiny jet locations effect in a sudden expansion duct for high-speed flow control using experimental and optimization methods.*
Meccanica, 56 (11).
pp. 1-26.
ISSN 0025-6455
E-ISSN 1572-9648

Aabid, Abdul and Khan, Sher Afghan and Baig, Maugal Ahmed Ali and Rao, K Srinivasa
(2021)
*Effect of control on the duct flow at high mach numbers.*
In: International Conference on Research and Advances in Mechanical Engineering(ICRAME 2020), 10th -11th December 2020, Hyderabad, India.

Aabid, Abdul and Khan, Sher Afghan and Baig, Maugal Ahmed Ali and Reddy, Avala Raji
(2021)
*Investigation of flow growth in a duct flows for higher area ratio.*
In: International Conference on Research and Advances in Mechanical Engineering(ICRAME 2020), 10th -11th December 2020, Hyderabad, India.

Abdul Aabid, Azmil Afifi and Khan, Sher Afghan
(2021)
*Numerical investigation of splitter plate effect on the bluff body using finite volume method.*
In: 2nd International Conference on Smart and Sustainable Developments in Materials, Manufacturing and Energy Engineering (SME), 22-23 December 2020, Nitte, India.

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, 38 (10.1016/j.matpr.2020.05.559).
pp. 2181-2190.
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

Ahmad, Mohamed Tarmizi and Jagannathan, A. and Abidin, Razali and Noordin, M. N.H. and Wan Ya’acob, Wan Mohd Hanif and Zhahir, Amzari and Azami, Muhammad Hanafi
(2021)
*Ballistic test investigation of hybrid rocket motor utilizing stearic acid biofuel with energetic additives for regression rate enhancement.*
In: 6th International Conference on Green Design and Manufacture 2020, IConGDM 2020, 23 - 24 July 2020, Arau, Perlis, Malaysia.

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
(2021)
*Jasad di bumi, minda di angkasa.*
e-estidotmy, 14 December 2021.
pp. 1-7.

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

## F

Faheem, Mohammed and Ridwan, R and Muneer, Rayid and Aneeque, Mohammed and Khan, Sher Afghan
(2021)
*Effect of expansion level on the flow development with sudden
expansion at high Mach numbers.*
In: 2nd International Conference on Smart and Sustainable Developments in Materials, Manufacturing and Energy Engineering, SME 2020, Nitte, Karnataka, India.

## 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

## I

Ismail, Atifatul Ismah and Khan, Sher Afghan and Rajendran, Parvathy and Sulaeman, Erwin
(2021)
*Effect of cavities in suddenly expanded flow at supersonic mach number.*
CFD Letters, 13 (9).
pp. 57-71.
ISSN 2180-1363

Ismail, Izham Izzat and Asmun, Siti Nurfaiqah and Abdullah, Nur Azam and Azami, Muhammad Hanafi and Nordin, Norhuda Hidayah
(2021)
*Numerical analyses for regression rate solid fuel doped with high entropy alloys in hybrid rocket motor.*
In: International Seminar on Aeronautics and Energy 2021 (ISAE 2021), 28 August 2021, Johor Bahru.
(Unpublished)

Ismail, Izham Izzat and Nordin, Norhuda Hidayah and Azami, Muhammad Hanafi and Abdullah, Nur Azam
(2022)
*Metals and alloys additives as enhancer for rocket propulsion: a review.*
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 90 (1).
pp. 1-9.
ISSN 2289-7879

Ismail, Izham Izzat and Rozainuddin, Nur Husnina Aufa and Nordin, Norhuda Hidayah and Azami, Muhammad Hanafi
(2022)
*Modelling of hybrid rocket flow-fields with computational fluid dynamics.*
CFD Letters, 3 (14).
pp. 53-67.
ISSN 2180-1363
E-ISSN 2811-3969

## J

Jaimon, Dennis Quadros and Khan, Sher Afghan and Aabid, Abdul and Alam, Mohammad Shohag and Baig, Muneer
(2021)
*Machine learning applications in modelling and analysis
of base pressure in suddenly, expanded flows.*
Aerospace, 8 (318).
pp. 1-23.
ISSN 2226-4310

## 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 Baig, Maughal Ahmed Ali and Ridwan, R and Rayid, Muneer and Suheel, J I and Faheem, Mohammed
(2021)
*Benefit of Mach number and expansion level on the flow development in a cylindrical tube diameter of 18 mm.*
In: 2021 International Conference on Technology Innovation in Mechanical Engineering, TIME 2021, 22 - 23 April 2021, Bhopal.

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 Ibrahim, Omar Mohamed and Aabid, Abdul
(2021)
*CFD analysis of compressible flows in a convergent-divergent nozzle.*
In: 2nd International Conference on Smart and Sustainable Developments in Materials, Manufacturing and Energy Engineering (SME), 22-23 December 2020, Nitte, India.

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 D. and Khan, Sher Afghan and Prashanth, T.
(2021)
*Study of buzz phenomenon in suddenly expanded flow
structure using experiments and visualization.*
Numerical Heat Transfer, Part B: Fundamentals An International Journal of Computation and Methodology.
pp. 1-18.
ISSN 1521-0626
E-ISSN 1040-7790

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

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

Ridwan, R and Chaudhary, Zakir Ilahi and Baig, Maugal Ahmed Ali and Suheel, J I and Khan, Sher Afghan and Faheem, Mohammed
(2022)
*Response of active control on the flow field of the duct pressure at supersonic Mach numbers.*
Materials Today, 48 (2).
pp. 1-8.
ISSN 2214-7853
(In Press)

Ridwan, R and Muhamad Zuraidi, Nur Husnina and Khan, Sher Afghan
(2022)
*Impact of cavity location on base pressure at Supersonic Mach 1.8.*
Journal of Mechanical Engineering Research and Development, 45 (2).
pp. 123-150.
ISSN 1024-1752

## 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.

## T

Turki, Al-Khalifa and Aabid, Abdul and Khan, Sher Afghan and Azami, Muhammad Hanafi and Baig, Muneer
(2021)
*Response surface analysis of nozzle parameters at supersonic flow through microjets.*
Australian Journal of Mechanical Engineering, 19 (3).
pp. 1-16.
ISSN 1448-4846
E-ISSN 2204-2253

## 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)