NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Model Preparation Area for High Reynolds Number Propulsion Airframe Integration Testing at the National Transonic FacilityNo abstract available
Document ID
20160007814
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Jones, Gregory S. (NASA Langley Research Center Hampton, VA, United States)
Flamm, Jeffrey D. (NASA Langley Research Center Hampton, VA, United States)
Acheson, Michael J. (NASA Langley Research Center Hampton, VA, United States)
Hudgins, Robert C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 22, 2016
Publication Date
January 4, 2016
Subject Category
Aerodynamics
Aircraft Design, Testing And Performance
Report/Patent Number
NF1676L-23362
Report Number: NF1676L-23362
Meeting Information
Meeting: AIAA SciTech Forum 2016
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 081876.02.07.02.01.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available