NASA Logo

NTRS

NTRS - NASA Technical Reports Server

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Drag Characteristics of Rectangular and Swept-back NACA 65-009 Airfoils Having Aspect Ratios of 1.5 and 2.7 as Determined by Flight Tests at Supersonic Speeds
Document ID
19930085725
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Alexander, Sidney R
Katz, Ellis
Date Acquired
August 16, 2013
Publication Date
February 24, 1947
Report/Patent Number
NACA-RM-L6J16
Report Number: NACA-RM-L6J16
Accession Number
93R15015
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available