Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76666/1/AIAA-46261-468.pd
The state-of-the-art methods in preliminary wing design are using models employing physics-based me...
This paper presents the development of an advanced, quasi-analytical method for aircraft wing weight...
This paper presents a semi-empirical method for the weight estimation of advanced transport aircraft...
A formula is derived to calculate structural wing mass. This formula can be applied to twin fuselage...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76882/1/AIAA-46232-142.pd
The Ultra-High Aspect Ratio Wing (UHARW) concept can improve the aircraft’s aerodynamic efficiency a...
The scope of the presented paper is to present a set of formulae that can be used to compute the mas...
This thesis presents the development, validation, and application of methods for the estimation of ...
© 2017 Elsevier Masson SAS In this paper, the current state of the art of aircraft wing mass estimat...
Abstract: The blended wing body (BWB) concept is one in which the payload is carried within the inne...
The implementation of key technologies in the initial stages of the aircraft wing design process has...
In the conceptual aircraft design phase, prediction of the empty weight typically relies on empirica...
The state-of-the-art methods in preliminary wing design are using models employing physics-based met...
State-of-the-art models in preliminary wing design apply physics-based methods for primary structure...
The implementation of the changes to the program for Wing Aeroelastic Design and the development of ...
The state-of-the-art methods in preliminary wing design are using models employing physics-based me...
This paper presents the development of an advanced, quasi-analytical method for aircraft wing weight...
This paper presents a semi-empirical method for the weight estimation of advanced transport aircraft...
A formula is derived to calculate structural wing mass. This formula can be applied to twin fuselage...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76882/1/AIAA-46232-142.pd
The Ultra-High Aspect Ratio Wing (UHARW) concept can improve the aircraft’s aerodynamic efficiency a...
The scope of the presented paper is to present a set of formulae that can be used to compute the mas...
This thesis presents the development, validation, and application of methods for the estimation of ...
© 2017 Elsevier Masson SAS In this paper, the current state of the art of aircraft wing mass estimat...
Abstract: The blended wing body (BWB) concept is one in which the payload is carried within the inne...
The implementation of key technologies in the initial stages of the aircraft wing design process has...
In the conceptual aircraft design phase, prediction of the empty weight typically relies on empirica...
The state-of-the-art methods in preliminary wing design are using models employing physics-based met...
State-of-the-art models in preliminary wing design apply physics-based methods for primary structure...
The implementation of the changes to the program for Wing Aeroelastic Design and the development of ...
The state-of-the-art methods in preliminary wing design are using models employing physics-based me...
This paper presents the development of an advanced, quasi-analytical method for aircraft wing weight...
This paper presents a semi-empirical method for the weight estimation of advanced transport aircraft...
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