NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
COMSAC: Computational Methods for Stability and ControlWork on stability and control included the following reports:Introductory Remarks; Introduction to Computational Methods for Stability and Control (COMSAC); Stability & Control Challenges for COMSAC: a NASA Langley Perspective; Emerging CFD Capabilities and Outlook A NASA Langley Perspective; The Role for Computational Fluid Dynamics for Stability and Control:Is it Time?; Northrop Grumman Perspective on COMSAC; Boeing Integrated Defense Systems Perspective on COMSAC; Computational Methods in Stability and Control:WPAFB Perspective; Perspective: Raytheon Aircraft Company; A Greybeard's View of the State of Aerodynamic Prediction; Computational Methods for Stability and Control: A Perspective; Boeing TacAir Stability and Control Issues for Computational Fluid Dynamics; NAVAIR S&C Issues for CFD; An S&C Perspective on CFD; Issues, Challenges & Payoffs: A Boeing User s Perspective on CFD for S&C; and Stability and Control in Computational Simulations for Conceptual and Preliminary Design: the Past, Today, and Future?
Document ID
20040084120
Acquisition Source
Langley Research Center
Document Type
Conference Proceedings
Authors
Fremaux, C. Michael
(NASA Langley Research Center Hampton, VA, United States)
Hall, Robert M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2004
Subject Category
Aircraft Stability And Control
Report/Patent Number
L-18378A/PT1
NASA/CP-2004-213028/PT1
Report Number: L-18378A/PT1
Report Number: NASA/CP-2004-213028/PT1
Meeting Information
Meeting: COMSAC: Computational Methods for Stability and Control
Location: Hampton, VA
Country: United States
Start Date: September 23, 2003
End Date: September 25, 2003
Sponsors: NASA Headquarters
Funding Number(s)
WORK_UNIT: WU 23-762-45-AF
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available