Purpose - Find optimal flight and design parameters for three objectives: minimum fuel consumption, Direct Operating Costs (DOC), and environmental impact of a passenger jet aircraft. ---
Approach - Combining multiple models (this includes aerodynamics, specific fuel consumption, DOC, and equivalent CO2 mass) into one generic model. In this combined model, each objective's importance is determined by a weighting factor. Additionally, the possibility of further optimizing this model by altering an aircraft's wing loading is analyzed. ---
Research limitations - Most models use estimating equations based on first principles and statistical data. ---
Practical implications - The optimal cruise altitude and speed for a specific objective can be approximated for any passenger jet aircraft. ---
Social implications - By using a simple approach, the discussion of optimizing aircraft opens up to a level where everyone can participate. ---
Value - To find a general answer on how to optimize aviation, operational and design-wise, by using a simple approach.
| Identifer | oai:union.ndltd.org:haw-hamburg.de/oai:Caers |
| Date | January 2019 |
| Creators | Caers, Brecht |
| Contributors | Scholz, Dieter |
| Publisher | Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences, |
| Source Sets | Hamburg Universtiy of Applied Sciences (HAW Hamburg) |
| Language | English |
| Detected Language | English |
| Type | Text, Master Thesis, doc-type:text, doc-type:masterThesis, info:eu-repo/semantics/masterThesis, info:eu-repo/semantics/publishedVersion, status-type:publishedVersion, info:eu-repo/semantics/publishedVersion |
| Format | text/html |
| Coverage | Hamburg, Germany |
| Rights | Copyright by author, CC BY-NC-SA, https://creativecommons.org/licenses/by-nc-sa/4.0, info:eu-repo/semantics/openAccess |
| Relation | info:eu-repo/semantics/dataset/doi/10.7910/DVN/DLZSDK, Digital Library - Projects & Theses - Prof. Dr. Scholz, http://library.ProfScholz.de |
Page generated in 0.0031 seconds