Development, Model Generation and Analysis of a Flying V Structure Concept

The Flying V, a concept aircraft configuration, has been proposed by Airbus and TU Berlin. The initial indications of potential improvements in performance over conventional aircraft gave rise to a continuation of the research. For this, the mass characteristics of the configuration must be explored. <br/><br/>A primary structure concept is...

Conceptual Design of Blended Wing Body Airliners Within a Semi-automated Design Framework

Blended wing body aircraft represent a paradigm shift in jet transport aircraft design. Stepping away from the conventional tube-and-wing philosophy, they promise benefits over existing or future conventional aircraft. The most significant challenge with the concept is the increased coupling between aircraft design disciplines that has...

Rudder Incorporated Winglet Design for Blended Wing Body Aircraft

Concern about the environmental footprint of aviation has re-sparked the interest in unconventional configurations, such as the blended wing body aircraft, BWB. While most research studies recognize the potential of the hybrid-body, they also list a number of challenges. Amongst these challenges is the need for adequate lateral-directional...

Effectiveness of Thrust Vectoring Control for Longitudinal Trim of a Blended Wing Body Aircraft

The application of thrust vectoring on civil transport aircraft has only been studied by a few individuals. Quantified investigations need to be carried out to search for the potential benefits of the application of thrust vectoring control on a civil transport aircraft. Blended Wing Body configuration is a novel aircraft concept. Due to the...

A hybrid method for the interior and exterior design of blended-wing-body cabins

Considering the fact that all large commercial aircraft have not changed significantly in their tube–and–wing shape during the past few decades, one would suggest that a completely different configuration is necessary to facilitate a new leap forward in aircraft performance. The blended–wing–body is potentially such an alternative configuration....

Design of Inlet for Boundary Layer Ingestion in a Blended Wing Body Aircraft

Boundary Layer Ingestion (BLI) is a concept in which the fuselage boundary layer is ingested by the engine to produce benefits like improved fuel efficiency, reduction of ram drag and lower structural weight of the configuration. Blended Wing Body (BWB) concept has been researched on and studied in various forms over the years as an efficient...

The Oval Fuselage: A New Structural Design Concept for Blended Wing Body Cabins

Faced with the decreasing fossil fuel reserves and the need to decrease its environmental footprint, the aviation industry is searching for alternative fuels and more fuel efficient engines and aircraft. With the current designs reaching their limits, the industry has turned its attention to the family of all lifting bodies. Particularly blended...

Multidisciplinary Design Optimization in the Conceptual Design Phase: Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy

Traditionally, the aircraft design process is divided into three phases: conceptual, preliminary and detailed design. In each subsequent phase, the fidelity of the analysis tools increases and more and more details of the design geometry are frozen. In each phase a number of design variants is generated, fully analyzing them with the tools...