Measuring Surface Geometry of Airplane Wing by Means of Two Methods

Journal Title: Aviation - Year 2009, Vol 13, Issue 2

Abstract

Determination of the geometry of aircraft surfaces has always been an extremely complicated task, though it is very important for the aerodynamic properties of the entire aircraft or its parts (like wings, body, rudders, etc.). Measurement of the geometrical properties of aircraft parts is especially difficult due to the smoothness of their surfaces. Here in this paper a short review of two methods of determining the shape of aircraft parts are given: one relies on determining point position by means of laser-based scanning and another relies on photogrammetry. A comparison of the results of both methods applied to the same aircraft element is also presented.

Authors and Affiliations

Domantas Bručas, Jūratė Sužiedelytė-Visockienė

Keywords

Related Articles

Measuring Surface Geometry of Airplane Wing by Means of Two Methods

Determination of the geometry of aircraft surfaces has always been an extremely complicated task, though it is very important for the aerodynamic properties of the entire aircraft or its parts (like wings, body, rudders,...

Orlaivio sparno geometrijos matavimas dviem metodais

Orlaivio paviršiaus geometrijos nustatymas visada buvo labai sudėtinga užduotis, nors tai labai svarbu orlaivio dalių (sparnų, liemens, vairų ir kt.) ar viso orlaivio aerodinaminių charakteristikų kontrolei. Nustatyti ge...

Analysis of Three Wing Sections

Three wing sections FX66-S-196VI, E603 and AH82-150A were analyzed. Measured data of these wing sections are published. First wing section was measured in Stuttgart University and in Delft University of Technology, when...

Fuselage Test of a Small Aircraft According to CS-23 Requirements

This article describes a static strength test of a fuselage of a small aircraft. Tests were done according to CS-23 requirements. The test program was firstly analysed and then a methodology of the entire test was create...

Model of Acoustic Emission Signal at the Prevailing Mechanism of Composite Material Mechanical Destruction

A model of acoustic emission signal formation at the prevailing mechanism of the destruction of composite materials is considered. The results of acoustic emission signal modelling are presented, taking into account the...

Download PDF file
  • EP ID EP83263
  • DOI 10.3846/1648-7788.2009.13.44-49
  • Views 91
  • Downloads 0

How To Cite

Domantas Bručas, Jūratė Sužiedelytė-Visockienė (2009). Measuring Surface Geometry of Airplane Wing by Means of Two Methods. Aviation, 13(2), 44-49. https://europub.co.uk/articles/-A-83263