Add to ORKGFigure of merit expressions for (a) fuel weight fraction in terms of range and aspect ratio and (b) propeller diameter in terms of power absorbed per blade have been derived. In the case of fuselage length heuristic approach has been adopted. Design and performance data of military propeller trainer airplanes, both piston props and turboprops, have been analyzed. Simple and effective correlations have been evolved for selecting fuel weight fraction, propeller diameter and fuselage length for baseline design configuration of military propeller trainer airplanes
The power speed reduction unit (PSRU) is the device that is loaded by the generating unit and the th...
For the sizing of an electric motor, the diameter and length of the installation space are important...
The tests on these model propellers were undertaken for the purpose of determining the performance c...
Different types of aeroplanes (small / large, propeller / jet) require their own type of preliminary...
The relevance of this study is predetermined by the improvement to the fuel efficiency of an aircraf...
Methods for estimating the approximate size, weight, and power of aircraft intended to meet specifie...
Four regional turboprop aircraft of different configuration are assessed on their key performance in...
Unmanned Aerial Vehicles (UAVs) are increasingly used in a wide variety of applications ranging from...
The paper concerns the conceptual design phase: definition of the airplane configuration according t...
This paper contains a theoretical study of various thermodynamic cycles for Gas-Turbine-propeller pr...
Subsequent to identifying the optimum engine cycle over a specified baseline design mission, one of ...
Three regional transport aircraft of different configuration are synthesized for the same design spe...
Calculations have been made t o find range? attainable by bombers of gross weights from l40,oOO to 3...
Computations are made of the performance of a propeller designed to develop 56 thrust horsepower at ...
The paper presents a new correlation-regression model of estimating the turbofan engine weight consi...
The power speed reduction unit (PSRU) is the device that is loaded by the generating unit and the th...
For the sizing of an electric motor, the diameter and length of the installation space are important...
The tests on these model propellers were undertaken for the purpose of determining the performance c...
Different types of aeroplanes (small / large, propeller / jet) require their own type of preliminary...
The relevance of this study is predetermined by the improvement to the fuel efficiency of an aircraf...
Methods for estimating the approximate size, weight, and power of aircraft intended to meet specifie...
Four regional turboprop aircraft of different configuration are assessed on their key performance in...
Unmanned Aerial Vehicles (UAVs) are increasingly used in a wide variety of applications ranging from...
The paper concerns the conceptual design phase: definition of the airplane configuration according t...
This paper contains a theoretical study of various thermodynamic cycles for Gas-Turbine-propeller pr...
Subsequent to identifying the optimum engine cycle over a specified baseline design mission, one of ...
Three regional transport aircraft of different configuration are synthesized for the same design spe...
Calculations have been made t o find range? attainable by bombers of gross weights from l40,oOO to 3...
Computations are made of the performance of a propeller designed to develop 56 thrust horsepower at ...
The paper presents a new correlation-regression model of estimating the turbofan engine weight consi...
The power speed reduction unit (PSRU) is the device that is loaded by the generating unit and the th...
For the sizing of an electric motor, the diameter and length of the installation space are important...
The tests on these model propellers were undertaken for the purpose of determining the performance c...