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
STATIC STABILITY AND CONTROL CHARACTERISTICS OF AN AIRPLANE MODEL WITH TAIL SURFACES OUTBOARD OF THE WING TIPS AT A MACH NUMBER OF 2.01Static stability and control characteristics of aircraft model with tail surfaces outboard of wing tips
Document ID
19630002676
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Driver, C. (NASA Langley Research Center Hampton, VA, United States)
Spearman, M. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-47
Report Number: NASA-TM-X-47
Accession Number
63N12552
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC SPEED
STABILITY AND CONTROL
WING TIP
TAIL SURFACE
STATIC STABILITY AND CONTROL

Related Records

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