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
Subsonic longitudinal aerodynamic characteristics of a 1/30-scale canard- airplane model having a wing with an aspect ratio of 6.0Longitudinal aerodynamic characteristics of 1/30 scale nuclear powered canard aircraft model having wing with aspect ratio 6.0
Document ID
19650017035
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Capone, F. J. (NASA Langley Research Center Hampton, VA, United States)
Igoe, W. B. (NASA Langley Research Center Hampton, VA, United States)
Re, R. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1962
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-668
Report Number: NASA-TM-X-668
Accession Number
65N26636
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRCRAFT MODEL
NUCLEAR POWER
CANARD
AERODYNAMIC CHARACTERISTICS
ASPECT RATIO

Related Records

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