NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Some comments on fuselage dragThe following areas relating to fuselage drag are considered: (1) fuselage fineness - ratio and why and how this can be selected during preliminary design; (2) windshield drag; (3) skin roughness; and (4) research needs in the area of fuselage drag.
Document ID
19760003915
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Roskam, J.
(Kansas Univ. Lawrence, KS, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: Proc. of the NASA, Ind., Univ., Gen. Aviation Drag Reduction Workshop
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N11003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available