Add to ORKGUnmanned aircraft wing structure strength testing needs to be carried out to verify unmanned aircraft wing structure strength calculation which is one of the requirementS needed to fulfill airworthiness requirement. This paper explainsaerodynamics load model used on the wing structural test and the design process of wing structural test using whiffletree. Wing structural testing on LAPAN Surveillance UAV (LSU)-05 will be used as study case. The load resulted from the whiffletree to represent aerodynamic load on LSU-05 compared to analytical calculation using Schrenk has less than 3 % error.Hlm.207-21
This work describes the aerodynamic performance of an aircraft model wing with RGV winglet. Ruppell’...
An Unmanned Surveillance Aerial Vehicle (USAV) is an air vehicle which is largely used for surveill...
stiffen in positive flight load direction, still remaining compliant in the opposite direction. Such...
Abstract. The aim of this project is to design, build and test an unmanned aircraft. The design of t...
ABSTRACTPrediction of an aerodynamic load acting on a wing or usually called wing loading becomes an...
This paper describes a parametric study on the design of the structural wing members of a weight-shi...
Design of the different wing designs which is fixed onto the flapping mechanism known as Ornithopter...
Extensive research of winglets has been done for many commercial high-speed aircraft applications in...
The Solar UAV is a multi-functional aerial vehicle that can be used in many applications. The obj...
abstract: This paper describes the development of a software tool used to automate the preliminary d...
Structural analysis is widely used in the analysis of aircraft structures with the common applicatio...
In this report, a quasi-static load analysis is conducted on an experimental light sport aircraft wi...
Through decade, the needs of the aircraft technologies are quite demanding and most of the demands c...
This paper describes a systematic technique for preliminary conceptual design of Unmanned Wing in Gr...
This paper presents the design and validation of a measurement system for aerodynamic characteristic...
This work describes the aerodynamic performance of an aircraft model wing with RGV winglet. Ruppell’...
An Unmanned Surveillance Aerial Vehicle (USAV) is an air vehicle which is largely used for surveill...
stiffen in positive flight load direction, still remaining compliant in the opposite direction. Such...
Abstract. The aim of this project is to design, build and test an unmanned aircraft. The design of t...
ABSTRACTPrediction of an aerodynamic load acting on a wing or usually called wing loading becomes an...
This paper describes a parametric study on the design of the structural wing members of a weight-shi...
Design of the different wing designs which is fixed onto the flapping mechanism known as Ornithopter...
Extensive research of winglets has been done for many commercial high-speed aircraft applications in...
The Solar UAV is a multi-functional aerial vehicle that can be used in many applications. The obj...
abstract: This paper describes the development of a software tool used to automate the preliminary d...
Structural analysis is widely used in the analysis of aircraft structures with the common applicatio...
In this report, a quasi-static load analysis is conducted on an experimental light sport aircraft wi...
Through decade, the needs of the aircraft technologies are quite demanding and most of the demands c...
This paper describes a systematic technique for preliminary conceptual design of Unmanned Wing in Gr...
This paper presents the design and validation of a measurement system for aerodynamic characteristic...
This work describes the aerodynamic performance of an aircraft model wing with RGV winglet. Ruppell’...
An Unmanned Surveillance Aerial Vehicle (USAV) is an air vehicle which is largely used for surveill...
stiffen in positive flight load direction, still remaining compliant in the opposite direction. Such...