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
SUPERSONIC AERODYNAMIC CHARACTERISTICS OF SOME SIMPLIFIED AND COMPLEX AIRCRAFT CONFIGURATIONS WHICH EMPLOY HIGHLY SWEPT TWISTED-AND-CAMBERED ARROW-WING PLANFORMSApplication of low drag-due-to-lift concept of linearized theory to the studies of twist and camber of isolated wing and wing-body configurations of supersonic aircraft
Document ID
19630029704
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fuller, D. E.
Mc Lean, F. E.
Date Acquired
August 1, 2013
Publication Date
January 1, 1963
Subject Category
Biosciences
Accession Number
63A25763
Distribution Limits
Public
Copyright
Other
Keywords
ARROW WING
MINIMUM DRAG
WING PLANFORM
LIFT-DRAG RATIO
AIRCRAFT DESIGN
SUPERSONIC AIRCRAFT

Available Downloads

There are no available downloads for this record.

Related Records

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