The study of aerodynamic characteristics is an important aspects in designing of an aircraft. The estimate of the lift and drag coefficients of the combination of wings and bodies at subsonic speeds. The calculation of these aerodynamic characteristics is a tedious workout in the preliminary design, as it has to be carried out repetitively for every different combination. A software for determining the wing-body combination lift and drag coefficients known as AC Estimator is being developed to serve as a solution to the tedious and time-consuming design method. The development and capabilities of this software to predict varieties aerodynamic characteristics with good accuracy as compared to manual calculation are being presented and disc...
This paper presents the development of an advanced, quasi-analytical method for aircraft wing weight...
Aerodynamic stability coefficients are necessary to be known before any unmanned aircraft flight is ...
This paper details a new software tool to aid in the conceptual design of blended-wingbody aircraft....
The present paper deals with the description of a software called ADAS (Aircraft Design and Analys...
The present paper deals with the description of a software called ADAS (Aircraft Design and Analysis...
An existing computer software package for the determination of lift, drag and pitching moment of the...
The methods for design of the dynamic aeroelastic characteristics of the aircraft relatively to the ...
Topics below are rather undesired, but important, outcome not yet completed research on the aircraft...
A computer program for determining the flight characteristics of light aircraft was developed. The p...
During the launching vehicles design and their optimization process, the implementing of aerodynamic...
This thesis presents the development, validation, and application of methods for the estimation of ...
A new method has been developed for calculating the pressure distribution and aerodynamic characteri...
OpenVSP is an aerodynamic solver developed by National Aeronautics and Space Administration (NASA) t...
There the new determination methods of stationary and non-stationary wave drag of revolution bodies ...
The state-of-the-art methods in preliminary wing design are using models employing physics-based met...
This paper presents the development of an advanced, quasi-analytical method for aircraft wing weight...
Aerodynamic stability coefficients are necessary to be known before any unmanned aircraft flight is ...
This paper details a new software tool to aid in the conceptual design of blended-wingbody aircraft....
The present paper deals with the description of a software called ADAS (Aircraft Design and Analys...
The present paper deals with the description of a software called ADAS (Aircraft Design and Analysis...
An existing computer software package for the determination of lift, drag and pitching moment of the...
The methods for design of the dynamic aeroelastic characteristics of the aircraft relatively to the ...
Topics below are rather undesired, but important, outcome not yet completed research on the aircraft...
A computer program for determining the flight characteristics of light aircraft was developed. The p...
During the launching vehicles design and their optimization process, the implementing of aerodynamic...
This thesis presents the development, validation, and application of methods for the estimation of ...
A new method has been developed for calculating the pressure distribution and aerodynamic characteri...
OpenVSP is an aerodynamic solver developed by National Aeronautics and Space Administration (NASA) t...
There the new determination methods of stationary and non-stationary wave drag of revolution bodies ...
The state-of-the-art methods in preliminary wing design are using models employing physics-based met...
This paper presents the development of an advanced, quasi-analytical method for aircraft wing weight...
Aerodynamic stability coefficients are necessary to be known before any unmanned aircraft flight is ...
This paper details a new software tool to aid in the conceptual design of blended-wingbody aircraft....