Design of a Short-To-Medium-Range Baseline Aircraft with an Entry into Service in 2035 for the HOPE Project
Open Access
Abstract
When assessing new technologies at the overall aircraft level, it is crucial to establish an appropriate benchmark to evaluate the resulting performance of the final concept aircraft. This publication defines a short-to medium-range baseline aircraft for entry into service in 2035, which serves as a benchmark for the HOPE project. This aircraft is sized using the Bauhaus Luftfahrt Aircraft Design Environment (BLADE), and its engine model is derived using the in-house tool Aircraft Propulsion System Simulation (APSS). The top-level aircraft requirements and technology assumptions for the entire project timeline are also defined and used for the baseline aircraft. Compared to a state-of-the-art aircraft (entry into service in 2015), the baseline aircraft consumes 21.4% less block fuel during the design mission and 20.9% less block fuel during the typical mission, since its operating empty mass is reduced by 13.6%, its aerodynamic performance is improved by 8.5%, and it has 6.4% more efficient engines.Keywords
Funding Information
- European Commission (101096275, 10068673)
- UK Research and Innovation (101096275, 10068673)
This publication has 12 references indexed in Scilit:
- The contribution of global aviation to anthropogenic climate forcing for 2000 to 2018Atmospheric Environment, 2021
- Definition and discussion of the intrinsic efficiency of wingletsINCAS BULLETIN, 2018
- Composite Cycle Engine Concept with Hectopressure RatioJournal of Propulsion and Power, 2016
- Distributed propulsion and ultra-high by-pass rotor study at aircraft levelThe Aeronautical Journal, 2015
- Methods for simulation and analysis of hybrid electric propulsion systemsCEAS Aeronautical Journal, 2014
- Reducing the weight of aircraft interiorsReinforced Plastics, 2014
- Civil Jet Aircraft Design1999
- Application of Oswatitsch's theorem to supercritical airfoil drag calculationJournal of Aircraft, 1993
- Analytic models for technology integration in aircraft design1990
- Design for performance1982