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
Transonic Aerodynamic and Trim Characteristics of a Multi-engine Delta-wing Airplane ModelWind tunnel testing of two and four engine models of delta wing aircraft for transonic drag rise increment and maximum lift-drag ratio comparison
Document ID
19660010447
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Foss, W. E., Jr. (NASA Langley Research Center Hampton, VA, United States)
Swihart, J. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 17, 1956
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L55I27B
Report Number: NACA-RM-L55I27B
Accession Number
66N19736
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DRAG
WIND TUNNEL
AIRCRAFT DESIGN
DELTA WING

Related Records

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