NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Application of a Knowledge-Based Optimization Method for Aerodynamic DesignThe current research is investigating the application of an optimization technique to an existing knowledge-based design tool. The optimization method, referred to as CODISC, helps improve the results from a knowledge-based design by eliminating the required advanced design knowledge, or help fine-tune a well-performing vehicle. Three CODISC designs are presented using a generic transonic transport, the Common Research Model (CRM). One design optimizes the baseline CRM to demonstrate the ability to improve a well-performing vehicle. Another design is performed from the CRM with camber and twist removed, which highlights the ability to use CODISC in the conceptual design phase. The final design implements laminar flow on the CRM, showing how CODISC can optimize the extent of laminar flow to find the best aerodynamic performance. All three CODISC designs reduced the vehicle drag compared to the baseline CRM, and highlight the new optimization technique’s versatility in the aircraft design industry.
Document ID
20200002562
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Lynde, Michelle N.
(NASA Langley Research Center Hampton, VA, United States)
Campbell, Richard L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 17, 2020
Publication Date
July 24, 2018
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NF1676L-29507
Report Number: NF1676L-29507
Meeting Information
Meeting: 2018 Royal Aeronautical Society Biennial Applied Aerodynamics Research Conference
Location: Bristol
Country: United Kingdom
Start Date: July 24, 2018
End Date: July 26, 2018
Sponsors: Royal Aeronautical Society
Funding Number(s)
WBS: 081876.02.07.02.01.05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CODISC
No Preview Available