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Conceptual Design and Structural Optimization of NASA Environmentally Responsible Aviation (ERA) Hybrid Wing Body Aircraft

https://doi.org/10.2514/6.2016-0229

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What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.2514/6.2002-2openalex-snapshot

Design of the Blended-Wing-Body subsonic transport

inferredcites →https://doi.org/10.2514/6.2003-3439openalex-snapshot

Thirty Years of Development and Application of CFD at Boeing Commercial Airplanes, Seattle

inferredcites →https://doi.org/10.2514/6.2004-4567openalex-snapshot

MDOPT - A Multidisciplinary Design Optimization System Using Higher Order Analysis Codes

inferredcites →https://doi.org/10.2514/6.2008-5840openalex-snapshot

Advanced PRSEUS Structural Concept Design and Optimization

inferredcites →https://doi.org/10.2514/6.2009-931openalex-snapshot

Hybrid Wing Body Configuration System Studies

inferredcites →https://doi.org/10.2514/6.2009-934openalex-snapshot

X-48B Flight Test Progress Overview

inferredcites →https://doi.org/10.2514/6.2010-657openalex-snapshot

Vehicle Sketch Pad: A Parametric Geometry Modeler for Conceptual Aircraft Design

inferredcites →https://doi.org/10.2514/6.2011-4047openalex-snapshot

Experimental Studies of Open Rotor Installation Effects

inferredcites →https://doi.org/10.2514/6.2012-1606openalex-snapshot

Finite Element Based HWB Centerbody Structural Optimization and Weight Prediction

inferredcites →https://doi.org/10.2514/6.2012-249openalex-snapshot

Improved Aerodynamic Analysis for Hybrid Wing Body Conceptual Design Optimization

inferredcites →https://doi.org/10.2514/6.2012-337openalex-snapshot

Hybrid Wing Body Configuration Scaling Study

inferredcites →https://doi.org/10.2514/6.2013-1688openalex-snapshot

Conceptual Design and Structural Analysis of an Open Rotor Hybrid Wing Body Aircraft

inferredcites →https://doi.org/10.2514/6.2015-2544openalex-snapshot

Update on HCDstruct - A Tool for Hybrid Wing Body Conceptual Design and Structural Optimization

inferredcites →https://doi.org/10.2514/6.2016-0007openalex-snapshot

Overview Of ERA Integrated Technology Demonstration (ITD) 51A Ultra-High Bypass (UHB) Integration for Hybrid Wing Body (HWB) (Invited)

inferredcites →https://doi.org/10.2514/masm16openalex-snapshot

54th AIAA Aerospace Sciences Meeting

inferredcites →https://doi.org/10.4135/9781483346526.n589openalex-snapshot

U.S. Department of Transportation

What points at this work

Incoming claims: where this work appears in other papers’ reference lists and arguments.

inferred← citeshttps://doi.org/10.2139/ssrn.5087765openalex-extracted

Data in Brief : Conceptual Design-Optimisation of a Subsonic Hydrogen-Powered Longrange Blended-Wing-Body Aircraft

inferred← citeshttps://doi.org/10.1007/s00158-024-03820-zopenalex-snapshot

Design optimization for the entire aircraft structure of civil aircraft with blended-wing-body layout

inferred← citeshttps://doi.org/10.2514/6.2016-0007openalex-snapshot

Overview Of ERA Integrated Technology Demonstration (ITD) 51A Ultra-High Bypass (UHB) Integration for Hybrid Wing Body (HWB) (Invited)

inferred← citeshttps://doi.org/10.2514/6.2016-4419openalex-snapshot

Structural Configuration Systems Analysis for Advanced Aircraft Fuselage Concepts

inferred← citeshttps://doi.org/10.2514/6.2018-0652openalex-snapshot

Model Uncertainty: A Challenge in Nonlinear Coupled Multidisciplinary System Design

inferred← citeshttps://doi.org/10.3390/machines13050373openalex-snapshot

Finite Element Analysis of Post-Buckling Failure in Stiffened Panels: A Comparative Approach

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