Please use this identifier to cite or link to this item: https://doi.org/10.48441/4427.3163
Publisher DOI: 10.5281/zenodo.18377808
Title: New Blended Wing Body (BWB) aircraft – is 50% fuel reduction a credible claim?
Language: English
Authors: Scholz, Dieter  
Keywords: aviation; airplane; air transport system; flying wing; hybrid flying wing; Blended Wing Body; BWB; Box Wing Aircraft; BWA; square-cube-law; preliminary sizing; aerodynamics; Computational Fluid Dynamics; CFD; flight mechanics; mass prediction; system integration; ground handling; emergency evacuation; fire suppression; wake turbulence; aerodrome; interior design; flight test; wind tunnel; stability; center of gravity; CG; ventilation; landing gear; cargo; ditching; Airbus; Boeing; VELA; AC20.30; JetZero; Natilus; Outbound Aerospace
Issue Date: 15-Jan-2026
Conference: Hamburg Aerospace Lecture Series 2026 
Abstract: 
Startup companies are convinced the Blended Wing Body (BWB) configuration will revolutionize flight and will use "up to 50% less fuel than today’s commercial jets" (www.jetzero.aero). The US-based companies are JetZero and Natilus. In December 2025, Outbound Aerospace had to shut down, running out of funding. In contrast: "Substantial fuel reduction cannot be expected for passenger aircraft" is the research result from a former HAW Hamburg project featuring a flying BWB demonstrator called AC20230 with a span of 3 m. The presentation guides the audience through the aeronautical disciplines and shows with real numbers and a few equations what to expect beyond unfounded promises and artist's impressions. However, a viable application could be a BWB tanker. Large parts of such an aircraft could remain unpressurized, and like the Northrop B2 bomber, the BWB offers low-observable (stealth) characteristics. Even more important: The U.S. Air Force needs a tanker replacement and has funds available. In 2023, the U.S. Air Force awarded a $235-million contract to JetZero to build a full-scale demonstrator by 2027 in partnership with Scaled Composites (Northrop Grumman).
URI: https://hdl.handle.net/20.500.12738/18731
DOI: 10.48441/4427.3163
Review status: Currently there is no review planned for this version
Institute: Forschungsgruppe Flugzeugentwurf und -systeme (AERO) 
Fakultät Luftfahrt- und Fahrzeugsysteme 
Type: Presentation
Additional note: SCHOLZ, Dieter, 2026. New Blended Wing Body (BWB) Aircraft – Is 50% Fuel Reduction a Credible Claim? Hamburg Aerospace Lecture Series (DGLR, RAeS, VDI, ZAL, HAW Hamburg), Hamburg, Germany, 15.01.2026. – Available from: https://doi.org/10.48441/4427.3163
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