Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76882/1/AIAA-46232-142.pd
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
This thesis presents the development, validation, and application of methods for the estimation of ...
The procedures used to establish the mass matrices characteristics for the fighter type wings studie...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76666/1/AIAA-46261-468.pd
A formula is derived to calculate structural wing mass. This formula can be applied to twin fuselage...
This article presents basic results from wing planform optimization for minimum drag with constraint...
The method of superposition of linearized conical flows has been applied to the calculation of the a...
A simplified lifting-surface theory that includes effects of compressibility and spanwise variation ...
A method is presented for calculating the lift and centers of pressure of wing-body and wing-body-ta...
The implementation of the changes to the program for Wing Aeroelastic Design and the development of ...
Spanwise lift distributions have been calculated for nineteen unswept wings with various aspect rati...
An improved method is presented for estimating the subsonic location of the semispan aerodynamic cen...
The greatest efficiency for a lifting surface at supersonic speeds, according to the theoretical con...
The scope of the presented paper is to present a set of formulae that can be used to compute the mas...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
This thesis presents the development, validation, and application of methods for the estimation of ...
The procedures used to establish the mass matrices characteristics for the fighter type wings studie...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76666/1/AIAA-46261-468.pd
A formula is derived to calculate structural wing mass. This formula can be applied to twin fuselage...
This article presents basic results from wing planform optimization for minimum drag with constraint...
The method of superposition of linearized conical flows has been applied to the calculation of the a...
A simplified lifting-surface theory that includes effects of compressibility and spanwise variation ...
A method is presented for calculating the lift and centers of pressure of wing-body and wing-body-ta...
The implementation of the changes to the program for Wing Aeroelastic Design and the development of ...
Spanwise lift distributions have been calculated for nineteen unswept wings with various aspect rati...
An improved method is presented for estimating the subsonic location of the semispan aerodynamic cen...
The greatest efficiency for a lifting surface at supersonic speeds, according to the theoretical con...
The scope of the presented paper is to present a set of formulae that can be used to compute the mas...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
This thesis presents the development, validation, and application of methods for the estimation of ...
The procedures used to establish the mass matrices characteristics for the fighter type wings studie...
DOI
Add to ORKG