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
Effects of modifications to a control surface on a 6-percent-thick unswept wing on the transonic control-surface flutter derivativesTransonic flutter derivatives for unswept wing control surface configurations determined by pressure cell measurements
Document ID
19660024053
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Gambucci, B. J. (NASA Ames Research Center Moffett Field, CA, United States)
Sorenson, R. M. (NASA Ames Research Center Moffett Field, CA, United States)
Wyss, J. A. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 2, 1958
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-A58B04
Report Number: NACA-RM-A58B04
Accession Number
66N33343
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
UNSWEPT WING
TRANSONIC FLUTTER
CONTROL SURFACE
PRESSURE MEASUREMENT
FLUTTER ANALYSIS

Related Records

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