Personal Info
- Country of residence: Australia
Information
Adnan Mahmoud Abdel-Fattah
Email: adfattah@gmail.com
Telephone: +61 2 8883 1698, Mob: +61 418 372 702
Date & Place of Birth: 12 March 1945, Burqa, Nablus, Palestine.
Citizenship: Australian since 1972, Palestinian by birth with Jordanian Passport.
Marital Status: Married - Two children.
Languages: Fluent in English and Arabic.
Ph.D - The University of Sydney, Australia - 1976-1978.
Granted the degree of Doctor of Philosophy Mechanical Engineering.
Thesis: The Refraction of Shock Waves at a Gaseous Interface.
M.Eng.Sc. - The University of Sydney, Australia - 1973-1975.
Granted the degree of (Master of Engineering Science) in Mechanical Engineering.
Thesis: An Experimental Investigation of Shock Wave Refraction at a CO2/He Interface.
B. Mech. Eng. - Cairo University, Egypt - 1965-1970.
Granted the degree of Bachelor in Mechanical Engineering - Power Section.
Burqa School – Burqa, Nablus, Palestine – 1952-1961
Primary ane Prepatory Levels.
Shuwaikh Secondary School – Kuwait - 1962-1965
General Secondary Cert. 1965.
EMPLOYMENT HISTORY
Research Experience
May, 1987 - June, 2007 Senior Research Scientist
Nov., 1982 - May, 1987Research Scientist
Defence Science and Technology OrganisationAeronautical and Maritime Research LaboratoryAirframes and Engines Division
Melbourne - Australia.
Experience gained in this period as a member of the propulsion aerodynamics group, included work on high pressure ratio thrust augmenting ejectors, confined jet mixing, aerodynamics of aircraft-engine run-up facilities, and aerodynamics of aircraft turbojet engine air intake duct.
My experimental investigation into the unsteady entrainment phenomena in relatively high pressure ratio thrust augmenting ejectors provided a valuable understanding of the complex acoustic interaction between a supersonic jet and a confining duct which is important to several aspects of jet mixing and entrainment such those occurring in ram rocket combustion chambers. The role of natural duct resonance in jet mixing has been identified, and correlations between initial jet conditions and ejector geometries have been developed. The discrete tone emission from both free and confined supersonic jets, and the effect of duct resonance on confined jet mixing in this high pressure application is beyond the experience of previous investigators. Refs (18, 19, 20, 22, 23, & 24)
Tests with unheated helium supersonic jets were carried out to help gain an understanding of the temperature effects by simulating the density differences between the core flow from a rocket motor and the co-flowing secondary air in the ejector duct. These confirmed the results of the actual rocket firing tests. These are yet to be published.
I have also performed an assessment study for multistage ejectors. This threw new light on the characteristics of these devices, and provided guidance as to their potential for practical applications. Refs (17, 21)
During this period I was also engaged in two major investigations of the aerodynamics of aircraft-engine ground run-up facilities upon request from RAAF. The first was to solve some operational problems by modifying an existing facility, and to assess a proposed design for the second. Both investigations were carried out with model scale testing in wind tunnel and with aircraft exhaust jet and propeller simulation. I was responsible as task manager and principle investigator to plan and supervise full scale aircraft tests in the facility, conduct or negotiate contract wind tunnel model testing of the facility. This required extensive liaison with RAAF personnel, commercial industrial and testing consultants. Refs (25, 26, 27, 28, and 29)
I was also responsible for the model scale development of an auxiliary intake system for an aircraft turbojet engine. This auxiliary system is to be only deployed during aircraft take-off and would be closed in flight. The program involved both static and tests with forward speed in the wind tunnel. Results of these test have shown that significant improvements in pressure recovery can be achieved without serious penalty in distortion levels at the engine face. Refs (30, 31, and 32).
Aug., 1978 - Oct., 1982 Research and Development Engineer.
James Howden Australia Pty. Ltd.
Sydney, Australia
More than four years R & D experience in the field of gas cleaning and air handling in mining and power generation industries in Australia. Responsibilities included planning, model design and supervision of its building, and conducting flow model testing of the equipment such as dust collection hoppers, flow straightening devices, and industrial fans. My contributions in this field are currently in use in three major power stations in Australia (Eraring, Bayswater and Mt. Piper).
During this period I have made several contributions to the low speed industrial axial flow fan design and technology. My major R & D achievement in this field was the development of a stabilising device which proved to be capable of eliminating the stall margin from any axial and mixed flow fan operation. Refs (11, 12, 13, 14, and 15). This fan stall alleviation device was patented world wide and is currently in use in several power stations in Australia.
1973 - 1978 Postgraduate Research Student
(Ph.D) 1978 The University of Sydney.
(M.Eng.Sc.)1976 The University of Sydney.
Four years experience with shock tube experiments and associated techniques, such as: Schlieren optics and photography, transducers, membrane technology (10 molecules thick) to separate two gases for shock refraction experiments. Design and construction of the experiments. Trouble shooting on the mechanical and electronic parts of the experiments. Calculations associated with data analysis.
Teaching Experience
Apr/78-Oct/79Part Time Lecturer
The University of Technology Sydney, previously known as “NSW Institute of Technology”.
Mech. Engineering Dept. Sydney.Australia.
Sep/73-Aug/78Part Time Tutor
The University of Sydney,
Mech. & Aero. Eng. Depts. Sydney, Australia.
May/71-Jul/73 Lecturer in Mathematics
Shuwaikh Industrial Training Centre.
United Nations Development Programs, (I.L.O).
Ministry of Labour - Kuwait
Subjects taught included Mathematics, Fluid Mechanics, Thermodynamics and Gas Dynamics.
Industrial Experience
Oct/73-Nov/74Laboratory Assistant.
Email Limited Sydney Australia.
Apr/73-Aug/73Quality Assurance Inspector.
Leyland Motor Corp. Sydney Australia.
Oct/70-Mar/71Refrigeration Engineer.
The Union of Commercial Companies - Kuwait.
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PUBLICATIONS
During my (Ph.D.) & (M. Eng. Sc.) Candidatures.
1. Abdel-Fattah, “An Experimental Investigation of Shock Wave Refraction at a
CO2/He Interface” Master of Engineering Science thesis. The University of
Sydney, 1975.
2. Abdel-Fattah L.F. Henderson & A. Lozzi. “Precursor Shock Waves at a Slow-Fast
Gas Interface”. J. of Fluid Mechanics., Vol. 76, p.157-176, 1976.
3. Abdel-Fattah & L.F. Henderson. “Shock Waves at a Fast-Slow Gas Interface”. J.
of Fluid Mechanics., Vol. 86, p.15-32, 1978.
4. Abdel-Fattah & L.F. Henderson. “Shock Waves at a Slow - Fast Gas Interface”. J.
of Fluid Mechanics., Vol. 89, p.79-95, 1978.
5. Abdel-Fattah, L.F. Henderson & A. Lozzi. “Cylindrical Precursor Shock Waves”.
Proceedings of the 14th IUTAM Congress, Delft - Netherlands, 1976.
6. Abdel-Fattah. “The Refraction of Shock Waves at a Gaseous Interface”. Doctor of
Philosophy, thesis. The University of Sydney, 1978.
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DURING JAMES HOWDEN AUSTRALIA EMPLOYMENT:
7. (James Howden Australia Pty ltd) B.A. Russel & A.M. Abdel- Fattah. Axial and Mixed Flow
Fans and Blowers. Patent granted in USA, UK, Canada, and World, 1982.
8. Abdel-Fattah. Eraring Fabric Filter Model Testing - Flow Distribution in Single
Cell. Report FA1, Sept., 1979.
9. Abdel-Fattah. Experimental Studies of Gas Flow Into Thimbles. Report FA12,
May, 1979.
10. Abdel-Fattah, “ Bayswater & Mt. Piper Fabric Filter Model Testing - Flow
Distribution Into a Single Cell”. Report FA8, Feb., 1982.
11. A.M. Abdel-Fattah Mixed Flow Fan Development, Stable Pressure - Volume
Characteristic. Report AA9, June, 1980.
12. A.M. Abdel-Fattah Mixed Flow Fan Development, Stable Pressure - Volume
Characteristic, Using a Closed Circulation Passage. Report AA10, Oct., 1980.
13. A.M. Abdel-Fattah Axial Flow Fan Development, Stable Pressure - Volume
Characteristic, Using a Closed Circulation Passage. Report AA11, Feb., 1981.
14. A.M. Abdel-Fattah Preliminary Report on Stable Pressure - Volume
Characteristic. Mixed Flow Impeller With Extended Blade Fixing. Report AA12,
Feb., 1981.
15. A.M. Abdel-Fattah Mixed Flow Fan Development, Effect of Vanes in the Closed
Circulation Passage. Report AA13, Feb., 1981.
16. A.M. Abdel-Fattah Tests on (Z 9) Impellers, Effects of Blade Width on
Performance. Report AA14, Sept
DURING AMRL EMPLOYMENT:
17. A.M. Abdel-Fattah "A Theoretical Study of Two Stage Thrust Augmenting
Ejectors". DSTO-ARL, Aero Prop Report 166, 1984.
18. A.M. Abdel-Fattah "Duct Resonance in High Pressure Ratio Thrust Augmenting
Ejectors". Proceedings of the 2nd Workshop on Wind Engineering and Industrial
Aerodynamics. CSIRO - Aug., 1985.
19. A.M. Abdel-Fattah & S. A. Fisher. "Duct Resonance and its Effect on Confined Jet Mixing". Proceedings of 12th Meeting of TTCP WTP-4, Cairns, Australia, Oct., 1986.
20. A.M. Abdel-Fattah "Discrete Tone Emission from High- Pressure Ratio Supersonic Jets from Convergent - Divergent Nozzles. Journal of the “American Insitute of Aeronautics and Astronautics”,(AIAA),Vol. 26, pp.283-291, March, 1988.
21. A.M. Abdel-Fattah "Two Stage Thrust Augmenting Ejectors - Subsonic Flow
Solution". Proceedings of the 9th Australasian Fluid Mechanics Conference,
Auckland - New Zealand, Dec., 1986.
22. S. A. Fisher & A.M. Abdel-Fattah. "Flow Measurements in High Pressure Ratio
Thrust Augmenting Ejectors". Proceedings of the 9th Australasian Fluid Mechanics Conference, Auckland - New Zealand, Dec., 1986.
23. A.M. Abdel-Fattah & S.C. Favaloro. "Duct Resonance and its Effect on the
Performance of High Pressure Ratio Axisymmetric Ejectors" Presented and
published in the proceedings of the 8th ISABE - Cincinnati, Ohio, USA. Paper
ISABE 87-7055, June 1987.
24. A.M. Abdel-Fattah & S. C. Favaloro. "Duct Resonance and its Effect on the
Performance of High Pressure Ratio Axisymmetric Ejectors". Journal of the “American Institute of Aeronautics and Astronautics”,(AIAA),, Vol. 26, pp.791-798, March, 1988.
25. A.M. Abdel-Fattah "Discrete Tone Generation from Free and Confined High
Pressure Ratio Axisymmetric Jets". Presented and published in the proceedings of
the 9th ISABE, Athens, Greece, Paper 89-075, pp.723-730, Sept.., 1989.
26. S. A. Fisher & A.M. Abdel-Fattah. "Aerodynamic Model Tests of Air Augmentors for F/A-18 Engine Run-up Facility at RAAF Williamtown". ARL-Aero-Prop TM.458,Dec.,1988.
27. S. A. Fisher & A.M. Abdel-Fattah. "Aerothermodynamics of Exhaust Augmentors
for Ground Running of F/A-18 Engines". Presented and published in the
proceedings of the Australian Aeronautical Conference, Melbourne, Oct., 1989.
28. A.M. Abdel-Fattah & W. H. Melbourne. "Wind Effects on P-3 Orion Engine Operation at RAAF Edinburgh Run-up Facility. Presented and published in the proceedings of The Australian Aeronautical Conference, Melbourne, Oct., 1989.
29. S. A. Fisher & A.M. Abdel-Fattah. "Aerothermodynamic Design Appraisal of
Noise Suppressors for F/A-18 Engine Run-up Facility at RAAF Williamtown"
DSTO - ARL, Prop. Report 177, Oct., 1990.
30. S. A. Fisher & A.M. Abdel-Fattah. "Aerothermodynamic Design of Noise
Suppressors for Ground Running Engines. Presented and published in the
proceedings of the 10th ISABE Nottingham - England, Sept., 1991.
31. A. M. Abdel-Fattah & S. A. Fisher. "An Auxiliary Intake System for an Unmanned Aircraft". Presented and published in the proceedings of the 10th ISABE Nottingham - England, Sept., 1991.
32. A. M. Abdel-Fattah. "Modification of Jindivik Air Intake Duct With an Auxiliary
Intake". ARL - PROP-TM-460, 1991
33. C & Y.Y. Link. "Low Speed Wind Tunnel Tests on Jindivik Air Intake Duct With and Without an Auxiliary Intake". ARL - PROP-TM 472, 472,1991.
34. A. M. Abdel-Fattah, M. F. Lee, and R. Carmichael, “A Louvred Auxiliary Air Intake System for a Turbojet Powered Target Aircraft”. Proceedings of the 11th Australasian Fluid Mechanics Conference. Hobart - Australia, 14 - 18 Dec,1992.
35. S. A. Fisher, A. M. Abdel-Fattah, and L, A. Challis, “Design Verification of Ground Run-Up Noise
Suppressors for Afterburning Engines”. Journal of Propulsion and Power, Vol. 9, pp. 628-635, Aug. - 1993.
36. A. M. Abdel-Fattah & P. C Frith, “Derivation of Axial Compressor Stage Characteristics from the Overall Performance Map.“ Proceedings of the 12th Australasian Fluid Mechanics Conference. Sydney - Australia, 10 - 15 Dec,,
1995
37. A. M. Abdel-Fattah, “Response of a Turbofan Engine Compression System to Disturbed Inlet Conditions“ Proceedings of the ASME TURBO EXPO 1996, Land, Sea & AIR, NEC Birmingham, UK, June 10 - 13 1996.
The paper has been selected as the best education paper presented at this international ASME - UK conference.
38.A. M. Abdel-Fattah, “Response of a Turbofan Engine Compression System to Disturbed Inlet Conditions”. Journal of Turbomachinery, October 1997, Vol. 119, 677-685
39.A. M. Abdel-Fattah, “Response of a Turboprop Compression System to Distorted Inlet Conditions”. Presented and published in the proceedings of the 15th ISABE Bangalore, India, September 2-7, 2001.
40.A. M. Abdel-Fattah & A. S. Vivian, “Development of the
SEMINARS & PRESENTATIONS:
1."Refraction of Shock Waves at a Gaseous Interface". Dept. of Mech. Eng. - Sydney University, 1-10-1975.
2."Thrust Augmenting Ejectors". Prop.Branch, A R L, Melbourne, 6-6-1984.
3."Flow Stability in Axial Flow Fans". Prop. Branch, A R L, Melbourne, 17-11-1985.
4."Duct Resonance and its Effect on Confined Jet Mixing". The 12th Meeting of TTCP WTP-4, Cairns, Australia, Oct., 1986.
5."Two Stage Thrust Augmenting Ejectors - Subsonic Flow Solution". The 9th Australasian Fluid Mechanics Conference, Auckland - New Zealand, Dec., 1986.
6.
"Ground Running Enclosures". Prop. Branch, A R L, Melbourne, 23-9-1987.
7.
"Unsteady Flow Phenomena in Confined Supersonic Jet Mixing". DIRECTOR'S SEMINAR, ARL, Melbourne, 4-8-1988.
8.
"Discrete Tone Generation from Free and Confined High Pressure Ratio Axisymmetric Jets". The 9th ISABE, Athens, Greece, Sept.., 1989.
9.
"Wind Effects on P-3 Orion Engine Operation at RAAF Edinburgh Run-up Facility. The Australian Aeronautical Conference, Melbourne, Oct., 1989.
10.
“Jindivik Intake Development”. Flight Mechanics and Propulsion
Divisional Seminar, ARL, Melbourne, 1-10-1991.
11.
“A Louvred Auxiliary Air Intake System for a Turbojet Powered Target Aircraft”. The 11th Australasian Fluid Mechanics Conference. Hobart - Australia, 14 - 18 Dec, 1992.
12.
“Derivation of Axial Compressor Stage Characteristics from the Overall Performance Map.“ The 12th Australasian Fluid Mechanics Conference. Sydney - Australia, 10 - 15 Dec, 1995.
13.
“Response of a Turbofan Engine Compression System to Disturbed Inlet Conditions”. Propulsion Seminar, 27-9-1996.
14.
“Response of a Turboprop Compression System to Distorted Inlet Conditions”. The proceedings of the 15th ISABE Bangalore, India, September 2-7, 200.
OTHER RELEVANT MATERIAL
1. Acted as a referee and reviewed papers in the field of Fluid Mechanics for Publication in international Journals such as Journal of the “American Insitute of Aeronautics and Astronautics”,(AIAA), and Journal of Experimental Thermal and Fluid Sciences.
2. Chairman of the Library Advisory Committee (LAC) at AMRL in
addition to being the Propulsion Branch representative on this committee.
3. Attended the following courses:
a) "Defence Organisational Study Seminar".
13-21/June/1984. Defence Training Centre, Melbourne - Australia.
b) "Management Principles for Engineers".
19-20/Feb/1987, Ordnance Factory, Maribyrnong, Melbourne - Australia.
c) "Staff Selection Course".
28-29/April & 4/May/1988. Defence Training Centre, Melbourne - Australia.
d) "Presentation Skills Course".
31/Jan & 6/Feb/1989. Royal Melbopurne Institute of Technology, M.I.T. - Melbourne –
Australia.
e) "Microcomputers for Scientists and Engineers".
22 & 29/June & 7/July/1989. Swinburn Institute of Tecnology, (S.I.T) - Melbourne -
Australia.
f) Develop collaborative activitiy between AMRL– DSTO and Sverdrup – AEDC, USA in the
field of aerodynamic modelling and code developments of the response of jet engine
compressor to distorted inlet conditions.
g) “Gas Turbine Performance”
A short course on gas turbines and jet engines in ongrounds facilities and those used in
commercial and military aircrafts.
Cranfield University – England, June 1996
Achievements and Awards
Invited as biographee in the American “Marquis Who’s Who in Science and Engineering”. My Biography continued to appear from 1997 to 2012. Well after my retirement in 2007.
Best Research Paper Award, from American Society for Mechanical Engineers (ASME) and Gas Turbine Insitute (GTI) for my research paper on modeling of aerodynamic stability of 3 spool turbofan jet engine.
This was the first award received from THE ASME by an Australian Scientist.
Research paper was presented at the ASME ASME TURBO EXPO 1996, Land, Sea
& AIR, NEC Birmingham, England., June 1996.
Award received at the ASME ASME TURBO EXPO 1997, Land, Sea & AIR, in Orlando, Florida, USA, June 1997.
Patent, USA, UK, Canada,, and World Wide, for an anti stall device capable of eliminating the stall margin from any axial and mixed flow fan operation, 1982.
The Australian Government Postgraduate Research Scholarship, (AGRS) to support my Ph.D candidature in Mechanical Engineering at Sydney University, 1976.
The Atlas Copco Prize for the best M.Eng.Sc. thesis submitted in Mechanical
Engineering at the University of Sydney during (1975).
The National Employment and Training Program Scholarship, NEAT to support my M.Eng.Sc. candidature at the University of Sydney, 1975.
The UNRWA (United Nations Relief and Work Agency) Scholarship,1965
to support my B. Mech. Eng. candidature at Cairo University. This was for being the 10th in the General Secondary Cert. Exam. (89.1%), (1965-1970)
- Years in active
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