This paper describes the development of a methodology for sizing
Blended-Wing-Body (BWB) transports and how the capabilities of the
Flight Optimization System (FLOPS) have been expanded using that
methodology. In this approach, BWB transports are sized based on
the number of passengers in each class that must fit inside the
centerbody or pressurized vessel. Weight estimation equations for
this centerbody structure were developed using Finite Element
Analysis (FEA). This paper shows how the sizing methodology has
been incorporated into FLOPS to enable the design and analysis of
BWB transports. Previous versions of FLOPS did not have the ability
to accurately represent or analyze BWB configurations in any
reliable, logical way. The expanded capabilities allow the design
and analysis of a 200 to 450-passenger BWB transport or the
analysis of a BWB transport for which the geometry is already
known. The modifications to FLOPS resulted in differences of less
than 4 percent for the ramp weight of a BWB transport in this range
when compared to previous studies performed by NASA and Boeing.
General
Is the information for this product incomplete, wrong or inappropriate?
Let us know about it.
Does this product have an incorrect or missing image?
Send us a new image.
Is this product missing categories?
Add more categories.
Review This Product
No reviews yet - be the first to create one!