NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Effect of twist and camber on the low-speed aerodynamic characteristics of a powered close-coupled wing-canard configurationA series of wind-tunnel tests were conducted in a V/STOL tunnel to determine the low-speed longitudinal aerodynamic characteristics of a powered close-coupled wing/canard fighter configuration. The data was obtained for a high angle-of-attack maneuvering configuration and a takeoff and landing configuration. The data presented in tabulated form are intended for reference purposes.
Document ID
19780018153
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Paulson, J. W., Jr. (NASA Langley Research Center Hampton, VA, United States)
Thomas, J. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-78722
Report Number: NASA-TM-78722
Accession Number
78N26096
Funding Number(s)
PROJECT: RTOP 505-11-23-05
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