ABSTRACTPrediction of an aerodynamic load acting on a wing or usually called wing loading becomes an important stage for structural analysis. Several methods have been used in estimating the wing loading. Schrenk approximation method is commonly used to achieve the fast estimation of lift distribution along wingspan, but in order to achieve a high level accuracy of aerodynamic prediction, computational fluid dynamics (CFD) with Navier Stokes-based equation can be used. LAPAN Surveillance UAV (LSU series) has been chosen to represent an aerodynamics analysis on generic small unmanned aircraft with twin-boom vertical stabilizer configuration. This study was focused to verify the Schrenk approximation method using high accuracy numerical simul...
The rocket development process goes through several stages with the aim of ensuring rocket performan...
Unmanned aircraft wing structure strength testing needs to be carried out to verify unmanned aircraf...
This bachelor´s thesis deals with aerodynamic analysis of unmanned aircraft and subsequent changes t...
Abstract: The preliminary analysis of wing of glider aircraftis presented. It gives a decisive consi...
Structural analysis is widely used in the analysis of aircraft structures with the common applicatio...
Pada tugas akhir ini dilakukan sebuah perancangan Pesawat Tanpa Awak (Unmanned Aerial Vehicle/ UAV)....
AbstractLSU-05 aircraft is one of the unmanned aerial vehicles (UAV), which is being developed by th...
Karakteristik aerodinamika adalah salah satu aspek yang dipertimbangkan dalam proses pemilihan konfi...
This paper describes the development of computer application for computing the wing lift distributio...
This paper deals with the aerodynamics of a box-wing (a type of closed-wing) aircraft. As demand for...
Small Unmanned Aerial Vehicle (SUAV) adalah pesawat terbang tanpa awak (PTTA) yang terbang pada keti...
Aerodynamic stability coefficients are necessary to be known before any unmanned aircraft flight is ...
The Solar Unmanned Aerial Vehicle (UAV) project was initiated by Defence Science Organization (DSO) ...
This thesis presents a study of aerodynamic of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UA...
Unmanned aerial vehicle (UAV) merupakan sebuah pesawat tanpa awak yang digerakkan tanpa pilot yang m...
The rocket development process goes through several stages with the aim of ensuring rocket performan...
Unmanned aircraft wing structure strength testing needs to be carried out to verify unmanned aircraf...
This bachelor´s thesis deals with aerodynamic analysis of unmanned aircraft and subsequent changes t...
Abstract: The preliminary analysis of wing of glider aircraftis presented. It gives a decisive consi...
Structural analysis is widely used in the analysis of aircraft structures with the common applicatio...
Pada tugas akhir ini dilakukan sebuah perancangan Pesawat Tanpa Awak (Unmanned Aerial Vehicle/ UAV)....
AbstractLSU-05 aircraft is one of the unmanned aerial vehicles (UAV), which is being developed by th...
Karakteristik aerodinamika adalah salah satu aspek yang dipertimbangkan dalam proses pemilihan konfi...
This paper describes the development of computer application for computing the wing lift distributio...
This paper deals with the aerodynamics of a box-wing (a type of closed-wing) aircraft. As demand for...
Small Unmanned Aerial Vehicle (SUAV) adalah pesawat terbang tanpa awak (PTTA) yang terbang pada keti...
Aerodynamic stability coefficients are necessary to be known before any unmanned aircraft flight is ...
The Solar Unmanned Aerial Vehicle (UAV) project was initiated by Defence Science Organization (DSO) ...
This thesis presents a study of aerodynamic of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UA...
Unmanned aerial vehicle (UAV) merupakan sebuah pesawat tanpa awak yang digerakkan tanpa pilot yang m...
The rocket development process goes through several stages with the aim of ensuring rocket performan...
Unmanned aircraft wing structure strength testing needs to be carried out to verify unmanned aircraf...
This bachelor´s thesis deals with aerodynamic analysis of unmanned aircraft and subsequent changes t...