Add to ORKGA computer program for determining the flight characteristics of light aircraft was developed. The parameters which were used in the computer program are defined. The accuracy of the system for various types of airfoils is analyzed and the airfoils for which the system does not provide adequate data are identified. The application of a computer program for predicting the fuselage characteristics is discussed. The assumptions and parameters of the fuselage characteristics program are explained. It is stated that the computer programs make it possible to determine the response of a light aircraft to a small disturbance given the geometric and inertial characteristics of the aircraft
The object of this report is to bring together the investigations of the various aerodynamic laborat...
v Methods for predicting the: perfornmnee, noise, weight, and cost of propellers for advanced genera...
The study of aerodynamic characteristics is an important aspects in designing of an aircraft. The es...
A computer program written in a table ""look-up'' format, is presented which provides a comprehensiv...
Methods for predicting the performance, noise, weight, and cost of propellers for advanced general a...
At the Fifth Space Congress, a method was [ presented for predicting the inviscid gas properties sur...
This Document Describes The Predesign Weight Estimation Method Of An Aircraft And A Computer Program...
A computer program developed to fit smooth surfaces to the component parts of three-dimensional airc...
A user's manual is presented for a computer program for predicting the performance (static, flight, ...
This Document Describes The Predesign Weight Estimation Method Of An Aircraft And A Computer Program...
A computer program developed to prepare wind tunnel generated airfoil data for input into helicopter...
An integrated system of computer programs has been developed for the design and analysis of superson...
Topics below are rather undesired, but important, outcome not yet completed research on the aircraft...
A computer technique to determine the mission radius and maneuverability characteristics of combat a...
A list of students involved in research on flight analysis and development is given along with abstr...
The object of this report is to bring together the investigations of the various aerodynamic laborat...
v Methods for predicting the: perfornmnee, noise, weight, and cost of propellers for advanced genera...
The study of aerodynamic characteristics is an important aspects in designing of an aircraft. The es...
A computer program written in a table ""look-up'' format, is presented which provides a comprehensiv...
Methods for predicting the performance, noise, weight, and cost of propellers for advanced general a...
At the Fifth Space Congress, a method was [ presented for predicting the inviscid gas properties sur...
This Document Describes The Predesign Weight Estimation Method Of An Aircraft And A Computer Program...
A computer program developed to fit smooth surfaces to the component parts of three-dimensional airc...
A user's manual is presented for a computer program for predicting the performance (static, flight, ...
This Document Describes The Predesign Weight Estimation Method Of An Aircraft And A Computer Program...
A computer program developed to prepare wind tunnel generated airfoil data for input into helicopter...
An integrated system of computer programs has been developed for the design and analysis of superson...
Topics below are rather undesired, but important, outcome not yet completed research on the aircraft...
A computer technique to determine the mission radius and maneuverability characteristics of combat a...
A list of students involved in research on flight analysis and development is given along with abstr...
The object of this report is to bring together the investigations of the various aerodynamic laborat...
v Methods for predicting the: perfornmnee, noise, weight, and cost of propellers for advanced genera...
The study of aerodynamic characteristics is an important aspects in designing of an aircraft. The es...