IIUM Repository

Dr Muhammad Hanafi Azami

Mechanical Engineering

International Islamic University Malaysia

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Latest Additions

  1. Mohamad Anuar, Mai Nurul Fareesya and Sujana, Mohammad Juani and Ismail, Izham Izzat and Azami, Muhammad Hanafi (2024) Experimental evaluation on the effects of energetic additives in the hybrid rocket fuel. Journal of Transport System Engineering, 11 (1). pp. 13-21. E-ISSN 2289–9790
  2. Mohd Zulkeple, Muhammad Fitri and Abu Talib, Abd Rahim and Harmin, Mohammad Yazdi and Saadon, Syamimi and Azami, Muhammad Hanafi and Yusaf, Talal (2024) Numerical investigation of heat transfer enhancement via dimpled target surface configuration and jet arrangement in impingement cooling. Journal of Aeronautics, Astronautics and Aviation, 56 (1S). pp. 93-106. ISSN 1990-7710
  3. Mohd Zulkeple, Muhammad Fitri and Abu Talib, Abd Rahim and Harmin, Mohammad Yazdi and Saadon, Syamimi and Azami, Muhammad Hanafi and Yusaf, Talal (2024) Comprehensive analysis of geometric hole designs and configurations in film cooling for gas turbine engines: a critical review. Journal of Aeronautics, Astronautics and Aviation, 56. pp. 187-218. ISSN 1990-7710
  4. Abd Razak, Najihah and Azami, Muhammad Hanafi (2024) Investigation on regression rate behavior of polylactic acid manufactured by fused deposition modelling for hybrid rocket motor. Journaal of Aeronautics, Astronautics and Aviation, 56 (1S). pp. 157-165. ISSN 1990-7710
  5. Azami, Muhammad Hanafi (2024) Euclid: misi merungkai misteri besar alam semesta. Risalah Falak. p. 14.
  6. Sabri, Muhammad Ezamuddin Ezzad and K., Togashi and Azami, Muhammad Hanafi (2023) Numerical analysis of fuel regression rate in Hybrid Rocket Motor with star shape port fuel grain. Perintis e-Journal, 13 (2). pp. 9-18. ISSN 2232-0725 E-ISSN 2232-0725
  7. Mohd Ali, Mohd Aizat Iz’aan and Razali, Muhammad Farhan and Azami, Muhammad Hanafi and Abdul Hamid, Ahmad Hussein (2023) Investigation on nozzle throat erosion in hybrid rocket motor due to nozzle expansion ratio. Journal of Aerospace Society Malaysia, 1 (2). pp. 1-8. E-ISSN 3009-0520
  8. Muhammad Yuhendri, Yoga Farhans and Nik Mohd, Nik Ahmad Ridhwan and Mat, Shabudin and Mohd Nasir, Mohd Nazri and Othman, Norazila and Mohd Rafie, Azmin Shakrine and Azami, Muhammad Hanafi (2023) Impact of cowl deflections on scramjet intake aerodynamics with shock-on-lip condition. Journal of Aeronautics, Astronautics and Aviation, 55 (3S). pp. 461-468. ISSN 1990-7710
  9. Alam, Jubayer Abdullah Rafiul and Abu Talib, Abd Rahim and Altarazi, Yazan Sofyan Mohammed and Yusaf, Talal and Azami, Muhammad Hanafi and Nik Mohd, Nik Ahmad Ridhwan (2023) Experimental investigation on gas turbine engine performance using alternative fuel. Journal of Aeronautics, Astronautics and Aviation,, 55 (3S). pp. 479-483. ISSN 1990-7710
  10. Sabri, Muhammad Ezamuddin Ezzad and Azami, Muhammad Hanafi and Abdullah, Nur Azam and Nordin, Norhuda Hidayah (2023) Investigation of regression rate end-burning typed hybrid rocket motor. Journal of Aeronautics, Astronautics and Aviation, 55 (3S). pp. 485-494. ISSN 1990-7710
  11. Azami, Muhammad Hanafi (2023) Starship bukti kemajuan teknologi aeorangkasa dunia. Berita Harian.
  12. Azami, Muhammad Hanafi and Abdullah, Nur Azam and Nordin, Norhuda Hidayah (2022) Investigation of regression rate end-burning typed hybrid rocket motor. In: The 6th Southeast Asia Workshop on Aerospace Engineering, Ho Chi Minh City University of Technology. (Unpublished)
  13. Sabri, Muhammad Ezamuddin Ezzad and Roslan, Mohammad Amirul Qayyum and Azami, Muhammad Hanafi and Salleh, Zuraidah (2023) Regression rate end-burning hybrid rocket motor doped with high entropy metallic additives. In: AIAA SciTech Forum, 23rd - 27th January 2023, National Harbor, MD, USA & Online.
  14. Ismail, Izham Izzat and Mohamad Jamil, Nur Arifah and Mohamad Anuar, Mai Nurul Fareesya and Azami, Muhammad Hanafi and Nordin, Norhuda Hidayah (2023) Investigation of hybrid rocket motor regression rate doped with high entropy metallic additives. In: AIAA SciTech Forum, 23rd - 27th January 2023, National Harbor, MD, USA & Online.
  15. Muhammad, Mohamad Amirul and Salleh, Zuraidah and Abd Hamid, Ahmad Hussein and Sujana, Mohammad Juani and Azami, Muhammad Hanafi and Haji Idris, Abd Halim (2022) Effects of propellant fabrication on the design for N-class KNSB solid rocket motor. International Transaction Journal of Engineering, Management, & Applied Sciences & Technologies, 13 (13). pp. 1-15. ISSN 2228-9860 E-ISSN 1906-9642
  16. Mohamad Jamil, Nur Arifah and Mohamaddiah, Ahmad Hadi and Azami, Muhammad Hanafi and Nordin, Norhuda Hidayah (2023) High entropy alloy as metal additive for hybrid rocket propellant. Materials Today: Proceedings, 75 (Part 1 (January 2023)). pp. 140-146. E-ISSN 2214-7853
  17. Shamsuddin, Mohd Firdaus and Azami, Muhammad Hanafi and Mohd Zaki, Hasan Firdaus and Abdullah, Nur Azam (2022) Effect of color contrast to the accuracy of SSD-MobileNetV2. International Journal of Intelligent Systems and Applications in Engineering, 10 (3). pp. 18-21. ISSN 2147-6799
  18. 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
  19. Ismail, Izham Izzat and Azami, Muhammad Hanafi (2022) Thrust chamber dynamic and propulsive performance of biofuels under detonation combustion. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 92 (2). pp. 71-93. ISSN 2289-7879
  20. 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

Most Viewed Items

Item titleViews
1Study of feasibility of pulse detonation engine powered by alternative fuels1132
2Inspection of supersonic flows in a CD nozzle using experimental method757
3Modelling of a three-shaft high-bypass-ratio engine performance and emission prediction using hydrogen fuels712
4Modelling of spray evaporation and penetration for alternative fuels703
5Investigation of aircraft engine performance utilizing various alternative fuels693
6Thermophysical behaviour of biofuel under detonation combustion686
7Metals and alloys additives as enhancer for rocket propulsion: a review639
8Modelling the performance of aero-gas turbine engine using algae-based biofuel with emission prediction633
9Experimental research of wall pressure distribution and effect of micro jet at Mach 1.5631
10Comparative study of alternative biofuels on aircraft engine performance621
11Comparative analysis of alternative fuels in detonation combustion620
12Comparison of aircraft engine performance and emission analysis using alternative fuels618
13Pulse detonation assessment for alternative fuels604
14Ballistic test investigation of hybrid rocket motor utilizing stearic acid biofuel with energetic additives for regression rate enhancement593
15Investigation of three-shaft high-bypass-ratio engine performance and emission prediction using alternative fuels553
16Performance and emission trade-off assessment for aero-gas turbine engine544
17Numerical analyses for regression rate solid fuel doped with high entropy alloys in hybrid rocket motor509
18Jasad di bumi, minda di angkasa487
19Modelling of hybrid rocket flow-fields with computational fluid dynamics451
20Effect of color contrast to the accuracy of SSD-MobileNetV2444
21High entropy alloy as metal additive for hybrid rocket propellant435
22James Webb space telescope - mencerap permulaan alam semesta414
23Thrust chamber dynamic and propulsive performance of biofuels under detonation combustion405
24Lucy - si pengembara asteroid Trojan388
25Regression rate end-burning hybrid rocket motor doped with high entropy metallic additives337
26Effects of propellant fabrication on the design for N-class KNSB solid rocket motor313
27Investigation of regression rate end-burning typed hybrid rocket motor295
28Investigation of hybrid rocket motor regression rate doped with high entropy metallic additives266
29Investigation of regression rate end-burning typed hybrid rocket motor220
30Experimental investigation on gas turbine engine performance using alternative fuel197