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Scopus Author ID: 57217137333

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M.Sherif Ahmed Soliman

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Russia

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Employment (1)

Novosibirsk State Technical University, Faculty of Aircraft: Novosibirsk, Novosibirsk Oblast, RU

PhD in Technical Sciences (Aircraft and Helicopter Construction)
Employment
Source: Self-asserted source
Mohamed Sherif E. Ahmed Soliman

Education and qualifications (1)

Novosibirskij gosudarstvennyj tehniceskij universitet Fakul'tet letatel'nyh apparatov: Novosibirsk, RU

Docent, Faculty member
Qualification
Source: Self-asserted source
Mohamed Sherif E. Ahmed Soliman

Works (13)

Building Berth for the Frame № 13

Unpublished
2017 | Other
DOI: 10.13140/RG.2.2.35953.68962
Contributors: M.Sherif Ahmed Soliman
Source: check_circle
DataCite

Calculation of the flight characteristics of the aircraft, AN-225

UnpublishedJournal of Aeronautics & Aerospace Engineering
2017 | Journal article
DOI: 10.13140/RG.2.2.22057.60004
Source: Self-asserted source
Mohamed Sherif E. Ahmed Soliman
grade
Preferred source (of 2)‎

Calculation of the flight characteristics of the aircraft, AN-225

Journal of Aeronautics & Aerospace Engineering
2017 | Journal article
DOI: 10.13140/RG.2.2.13374.08000
Source: Self-asserted source
Mohamed Sherif E. Ahmed Soliman
grade
Preferred source (of 2)‎

Proposal Decision for "Prove Mathematically and Graphically that, the required thrust does not equal to the force of resistance for the aircraft and the car?"

Unpublished
2017 | Other
DOI: 10.13140/RG.2.2.35479.37288
Contributors: M.Sherif Ahmed Soliman
Source: check_circle
DataCite

Proposal Decision for "Prove Mathematically and Graphically that, the required thrust does not equal to the force of resistance for the aircraft and the car?"

Unpublished
2017 | Other
DOI: 10.13140/RG.2.2.16657.43365
Contributors: M.Sherif Ahmed Soliman
Source: check_circle
DataCite

Prove Mathematically and Graphically that the required thrust does not equal to the force of resistance for the aircraft and the car?

Unpublished
2017 | Other
DOI: 10.13140/RG.2.2.22529.45926
Contributors: M.Sherif Ahmed Soliman
Source: check_circle
DataCite

“Assembly Process in Aircraft Construction”

Unpublished
2017 | Other
DOI: 10.13140/RG.2.2.19305.08802
Contributors: M.Sherif Ahmed Soliman
Source: check_circle
DataCite

The Effect of Supersonic Flows on Different Profiles of Aircraft Wings

The Global Journal of Researches in Engineering (GJRE)
2017-07-31 | Journal article
Source: Self-asserted source
Mohamed Sherif E. Ahmed Soliman

Automatic Control of the Electrical Autopilot of the Aircraft

World Journal of Engineering Research and Technology
2017-05-17 | Journal article
DOI: 10.13140/RG.2.2.23832.80640
Source: Self-asserted source
Mohamed Sherif E. Ahmed Soliman

Problems in Flight Dynamics & Its Solutions

World Journal of Engineering Research and Technology
2017-05-17 | Journal article
DOI: 10.13140/RG.2.2.32221.41443
Source: Self-asserted source
Mohamed Sherif E. Ahmed Soliman
grade
Preferred source (of 2)‎

Assembly Process in Aircraft Construction

Unpublished
2017-05-16 | Patent
DOI: 10.13140/RG.2.2.15346.71360
Source: Self-asserted source
Mohamed Sherif E. Ahmed Soliman
grade
Preferred source (of 2)‎

BUILDING BERTH

Unpublished
2017-05-16 | Patent
DOI: 10.13140/RG.2.2.34721.61282
Source: Self-asserted source
Mohamed Sherif E. Ahmed Soliman
grade
Preferred source (of 2)‎

Calculation of the Flight Characteristics of the Aircraft, AN-225

Journal of Aeronautics & Aerospace Engineering
2017-03-10 | Journal article
DOI: 10.13140/RG.2.2.16690.20165
Source: Self-asserted source
Mohamed Sherif E. Ahmed Soliman
grade
Preferred source (of 2)‎
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