Zobrazeno 1 - 10
of 522
pro vyhledávání: '"High angle of attack"'
Autor:
Li Bin, Guo Zhengyu
Publikováno v:
Hangkong bingqi, Vol 30, Iss 6, Pp 37-43 (2023)
The heading reversal of air-to-air missile is designed based on relaxed static stability and aerodynamic torque generated by static instability of air-to-air missile, and the kinematic sign is proposed. The slender body theory and the viscous crossfl
Externí odkaz:
https://doaj.org/article/91840d2b464e455e8f8bc4ce08f728c7
Publikováno v:
Hangkong gongcheng jinzhan, Vol 13, Iss 3, Pp 74-85 (2022)
The close combat in air battle is still inevitable in future.The accurate and agile nose-pointing capability at high-angle-of-attack is still essential and significant for fighter to survive and gain air superiority.According to the high-angle-of-att
Externí odkaz:
https://doaj.org/article/76705c5c256148f6b0cb0a3ceaf7cd40
Publikováno v:
Aerospace, Vol 11, Iss 1, p 70 (2024)
The upset state is an unexpected flight state, which is characterized by an unintentional deviation from normal operating parameters. It is difficult for the pilot to recover the aircraft from the upset state accurately and quickly. In this paper, an
Externí odkaz:
https://doaj.org/article/e1b13df2b9bf406993a5ed7be699d00b
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 15, Iss 3, Pp 943-958 (2022)
To understand the jet flow characteristics of turbofan separate exhaust system, a parametric design method based on the initial Class Shape Transformation function was developed. HBPR and UHBPR turbofan separate exhaust systems were designed. Further
Externí odkaz:
https://doaj.org/article/7a98310f82f443b79acf2dc1a6ee1239
Publikováno v:
IEEE Access, Vol 10, Pp 36373-36384 (2022)
This paper investigates an intelligent method for the motion control of a cable-driven parallel suspension system (CDPSS) in wind tunnel tests, especially at high angles of attack, which is characterized by unsteady and nonlinear aerodynamics. Consid
Externí odkaz:
https://doaj.org/article/e46c7f04e26d416d96e4fc8aff286b87
Publikováno v:
Hangkong gongcheng jinzhan, Vol 12, Iss 6, Pp 79-85 (2021)
The landing maneuver of aircraft is considered to be a feasible way to solve the problem of ultra short distance,precise landing of carrier based fixed wing aircraft. The existing researches mainly focus on aerodynamic modeling,nominal landing trajec
Externí odkaz:
https://doaj.org/article/3f776d8c508244e39d52ad004b6a1850
Akademický článek
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Akademický článek
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Akademický článek
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Publikováno v:
Aerospace, Vol 10, Iss 9, p 746 (2023)
This paper introduces a generic model for the study of aerodynamic behaviour relevant to fifth-generation high-performance aircraft. The model design is presented, outlining simplifications made to retain the key features of modern high-performance v
Externí odkaz:
https://doaj.org/article/8add2cf1ec6f4334b972047f4ca2282a