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Modern Aircraft Design of Sukhoi Su-27 (as should be) | Design Analysis and Aspect Ratio Review

Inspired by perfect design of Sukhoi Su-27 fighter aircraft, I study and analyze the design of the aircraft to find the advantages of the aircraft. I am very excited that Su-27 is an advance aircraft, compact in design, better in aerodynamic and super maneuverable. So in the basis of Sukhoi Su-27 design, I’d love to develop advanced design of aircraft for next generation fighter aircraft. Proper methodology is applied in designing an experimental aircraft design with many parameters as described. But don’t ask me if I graduated of Aviation or Aeronautical and even Aerospace. All my design is based on analysis how an aircraft design should be. My focus is to study and analyze perfect design of Sukhoi Su-27, the super maneuverable fighter, for 6th generation aircraft. I don’t have enough time to design new aircraft almost from the beginning. So the best way to develop new aircraft design is to analyze an existing aircraft design, find the advantages, and finally implement to develop the ...

Trapezoidal Wings of Sukhoi Su-57 Design (should be) for 6th Generation Upgrade | Design Analysis and Configuration | Aspect Ratio Review

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A trapezoidal wing is a straight-edge or sweep-edge and tapered wing planform. It may have any aspect ratio and may or may not be swept . T he t rapezoidal wing we’ll talk about  in this design analysis and configuration is trapezoidal in which leading - edge swe ep back while trailing - edge sweep forward : a trapezoidal wing of Sukhoi Su-57 combined with LERX as well as adding tail as should be. And note that this article will be updated regularly according to the progress of my analysis, and will be equipped with more descriptions, illustrations and design analysis, as well as equations of the parameters. These are the advantages and disadvantages of such trapezoidal wings configuration: Advantages: Ÿ   Better performance than d elta wings at transonic   speed   and during transition to and from supersonic conditions. Ÿ   D o not require upwards deflection of the trailing-edge control surfaces for pitch control and therefore do n...