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  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.

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Showing 1 to 3 of 3 (0.096 seconds)

Spelling suggestions: "subject:"ighlight characteristics"" "subject:"highlight characteristics""

1

Posouzení letových vlastností a zatížení malého sportovního letounu po modifikaci pohonné jednotky / Engine Rotax 915 for small light aircraft

Hrabovský, Matúš January 2020 (has links)
The thesis deals with the issue of replacement of the Rotax 912 ULS engine with the Rotax 915 iSc3 B engine and its impact on flight performance, characteristics and airframe loads of the WT 9 Dynamic. For accomplish better maneuverability tail surfaces are enlarged. Both versions of airplane with different engines and tails surfaces are quantified with respect to airframe loads and flight characteristics. The output of the diploma thesis can be used for strength design of airplane structure and stress tests of the new modification of the WT 9 Dynamic aircraft.
2

Stabilita a řiditelnost letounu Z-143 s výkonnější pohonnou jednotkou / Stability and controllability of the Z-143 airplane with a more powerful engine

Kochtík, Martin January 2017 (has links)
The thesis deals with the calculation and evaluation of the flight characteristics of the aeroplane Z 143 with the power unit Lycoming AEIO-580-B1A. The first part of the text focuses on a general description of the aircraft, its geometric characteristics and calculation of mass and aerodynamic characteristics. In terms of flight performance there are compared the values for contemporary model and developmental aircraft with a more powerful engine. Another part of the work deals with the calculation of properties in terms of stability and manageability. In this section regards the determination of the results of the flight characteristics and their assessment of whether they comply. In the end I discuss the individual results and comment the possible recommendations on correction or improvement of these properties.
3

Sklandytuvo svorio centro padėties įtakos skrydžio charakteristikai analizė / The analysis of the glider gravity center influence to the flight characteristics

Jurkštas, Kęstutis 30 August 2011 (has links)
Standartinės klasės sklandytuvo SZD – 48 – 3 “Jantar Standard 3” optimalios svorio centro padėties radimas. Pateikta skaičiavimai optimaliai svorio centro padėčiai surasti bei jos kitimas kintant greičiui. / The objective of this Master thesis is to investigate the glider gravity centre influence to the flight characteristics. Analyzing Frank Irving method, to find optimal centre of gravity. The subject of thesis is Standard class glider SZD – 48 – 3 “Jantar Standard 3”and calculation of optimal center of gravity position.
Transport Engineering
Svorio centras
Optimali padėtis
Skrydžio charakteristika
Standartinės klasės sklandytuvas
Skaičiavimas
Center of gravity
Optimal position
Flight characteristics
Standard class glider
Calculation

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