Ice accretion can significantly alter jet airplane transient response and has long been considered an important risk to aircraft aviation safety. This paper presents an overview of studies investigating the impact of ice accumulation on aviation dynamics. Methods for obtaining iced aircraft aerodynamic data, flight interactive computational methods for iced airframe, consequences of ice coalescence on aircraft structural rigidity but also flight efficiency, and aircraft icing envelope system protection adaptation have all been given special attention. To put the multiple test results into context, appropriate statistics of the critical indicators and constraints implicated in analytical and numerical icing modelling techniques, as well as key airflow testing simulation parameters and governing stream thermodynamics concerns, are presented. The precise analyses, evaluation, and comparisons of a large series of research dimensions of diverse types of mostly virtual in-flight and ground ice accretions follow, supplemented where acceptable by similar measured data for other comparable forms of contaminations and/or interruptions.
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2 August 2024
PROCEEDINGS OF THE FOURTH INTERNATIONAL CONFERENCE ON ADVANCES IN MANUFACTURING TECHNOLOGY: ICAMT2022
25–26 March 2022
Chennai, India
Research Article|
August 02 2024
Air craft aerodynamics and ice accretion effects Available to Purchase
Harishkumar Muddisetty;
Harishkumar Muddisetty
1
M.Sc Engineering in Mechanical Manufacture,Wrexham Glyndwr University
, Mold Road, Wrexham, United Kingdom
-LL 11 2AW
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Sai Ashish Kumar Karanam;
Sai Ashish Kumar Karanam
2
Department of Mechanical Engineering, Au College of Engineering, Andhra University
, Visakhapatnam 530003, India
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Ronald Miguel Hernandez Vasquez;
Ronald Miguel Hernandez Vasquez
3
Departmento de Educacion, Universidad Catolica Santo Toribio de Mogrovejo
, Chiclayo, Peru, Brazil
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Femmy Effendy;
Femmy Effendy
4
Universitas Pendidikan Indonesia
, Jawa Barat 40154, Indonesia
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Gnanel Muthu;
Gnanel Muthu
5
Department of Chemical Technology, Rajalakshmi Institute of Technology
, Chennai, Tamilnadu, India
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Chandra Kumar Dixit;
Chandra Kumar Dixit
a)
6
Department of Physics, Dr. Shakuntala Misra National Rehabilitation University
, Lucknow 226017. Uttar Pradesh, India
a)Corresponding author: [email protected]
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Sendilvelan Subramanian
Sendilvelan Subramanian
7
Department of Mechanical Engineering, Dr. M G R Educational and Research Institute
, Maduravoyal, Chennai 600095, Tamilnadu, India
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Harishkumar Muddisetty
1
Sai Ashish Kumar Karanam
2
Ronald Miguel Hernandez Vasquez
3
Femmy Effendy
4
Gnanel Muthu
5
Chandra Kumar Dixit
6,a)
Sendilvelan Subramanian
7
1
M.Sc Engineering in Mechanical Manufacture,Wrexham Glyndwr University
, Mold Road, Wrexham, United Kingdom
-LL 11 2AW
2
Department of Mechanical Engineering, Au College of Engineering, Andhra University
, Visakhapatnam 530003, India
3
Departmento de Educacion, Universidad Catolica Santo Toribio de Mogrovejo
, Chiclayo, Peru, Brazil
4
Universitas Pendidikan Indonesia
, Jawa Barat 40154, Indonesia
5
Department of Chemical Technology, Rajalakshmi Institute of Technology
, Chennai, Tamilnadu, India
6
Department of Physics, Dr. Shakuntala Misra National Rehabilitation University
, Lucknow 226017. Uttar Pradesh, India
7
Department of Mechanical Engineering, Dr. M G R Educational and Research Institute
, Maduravoyal, Chennai 600095, Tamilnadu, India
a)Corresponding author: [email protected]
AIP Conf. Proc. 2937, 020041 (2024)
Citation
Harishkumar Muddisetty, Sai Ashish Kumar Karanam, Ronald Miguel Hernandez Vasquez, Femmy Effendy, Gnanel Muthu, Chandra Kumar Dixit, Sendilvelan Subramanian; Air craft aerodynamics and ice accretion effects. AIP Conf. Proc. 2 August 2024; 2937 (1): 020041. https://doi.org/10.1063/5.0218223
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