METHODS FOR THE STUDY OF FLIGHT LOADS OF AIRCRAFT

Background. As is known, the rocket must have sufficient strength and withstand all loads during operation. The test of the design of the rocket for strength can be carried out in two ways: on workloads or by calculated loads exceeding workers. When studying the loads acting on the rocket, special...

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Autores principales:	A.D. Tulegulov, D.S. Yergaliyev, B.S. Beisembayeva, D.V. Zuev
Formato:	article
Lenguaje:	EN RU
Publicado:	Penza State University Publishing House 2021
Materias:	strength load test engine design Motor vehicles. Aeronautics. Astronautics TL1-4050
Acceso en línea:	https://doaj.org/article/0473c243e5384bc59b18fc15a2719cde
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spelling	oai:doaj.org-article:0473c243e5384bc59b18fc15a2719cde2021-12-01T11:52:52ZMETHODS FOR THE STUDY OF FLIGHT LOADS OF AIRCRAFT10.21685/2307-4205-2021-3-62307-4205https://doaj.org/article/0473c243e5384bc59b18fc15a2719cde2021-11-01T00:00:00Zhttps://doaj.org/toc/2307-4205Background. As is known, the rocket must have sufficient strength and withstand all loads during operation. The test of the design of the rocket for strength can be carried out in two ways: on workloads or by calculated loads exceeding workers. When studying the loads acting on the rocket, special attention should be paid to flight loads. Load in flight depends on the characteristics of the rocket engine, the nature of the air flow rocket and the dynamics of the movement. Materials and methods. The calculation is made at maximum high-speed pressure in the exit zone of two-stage liquid fuels into the rocket housing. We can say that the head of the rocket is made in the form of a sharp cone Results. As a result of research, it is possible to note the fact that in training with reinforcement an agent interacts with the environment, taking actions and receives a reward for these actions. Conclusions. With any calculation of testing tests, errors will be selected when choosing a design selection circuit. To test the results of the calculation, it is sufficient to test the structure before it is destruction, with a uniform increase in the load.A.D. TulegulovD.S. YergaliyevB.S. BeisembayevaD.V. ZuevPenza State University Publishing HousearticlestrengthloadtestenginedesignMotor vehicles. Aeronautics. AstronauticsTL1-4050ENRUНадежность и качество сложных систем, Iss 3 (2021)
institution	DOAJ
collection	DOAJ
language	EN RU
topic	strength load test engine design Motor vehicles. Aeronautics. Astronautics TL1-4050
spellingShingle	strength load test engine design Motor vehicles. Aeronautics. Astronautics TL1-4050 A.D. Tulegulov D.S. Yergaliyev B.S. Beisembayeva D.V. Zuev METHODS FOR THE STUDY OF FLIGHT LOADS OF AIRCRAFT
description	Background. As is known, the rocket must have sufficient strength and withstand all loads during operation. The test of the design of the rocket for strength can be carried out in two ways: on workloads or by calculated loads exceeding workers. When studying the loads acting on the rocket, special attention should be paid to flight loads. Load in flight depends on the characteristics of the rocket engine, the nature of the air flow rocket and the dynamics of the movement. Materials and methods. The calculation is made at maximum high-speed pressure in the exit zone of two-stage liquid fuels into the rocket housing. We can say that the head of the rocket is made in the form of a sharp cone Results. As a result of research, it is possible to note the fact that in training with reinforcement an agent interacts with the environment, taking actions and receives a reward for these actions. Conclusions. With any calculation of testing tests, errors will be selected when choosing a design selection circuit. To test the results of the calculation, it is sufficient to test the structure before it is destruction, with a uniform increase in the load.
format	article
author	A.D. Tulegulov D.S. Yergaliyev B.S. Beisembayeva D.V. Zuev
author_facet	A.D. Tulegulov D.S. Yergaliyev B.S. Beisembayeva D.V. Zuev
author_sort	A.D. Tulegulov
title	METHODS FOR THE STUDY OF FLIGHT LOADS OF AIRCRAFT
title_short	METHODS FOR THE STUDY OF FLIGHT LOADS OF AIRCRAFT
title_full	METHODS FOR THE STUDY OF FLIGHT LOADS OF AIRCRAFT
title_fullStr	METHODS FOR THE STUDY OF FLIGHT LOADS OF AIRCRAFT
title_full_unstemmed	METHODS FOR THE STUDY OF FLIGHT LOADS OF AIRCRAFT
title_sort	methods for the study of flight loads of aircraft
publisher	Penza State University Publishing House
publishDate	2021
url	https://doaj.org/article/0473c243e5384bc59b18fc15a2719cde
work_keys_str_mv	AT adtulegulov methodsforthestudyofflightloadsofaircraft AT dsyergaliyev methodsforthestudyofflightloadsofaircraft AT bsbeisembayeva methodsforthestudyofflightloadsofaircraft AT dvzuev methodsforthestudyofflightloadsofaircraft
_version_	1718405215493816320

METHODS FOR THE STUDY OF FLIGHT LOADS OF AIRCRAFT

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