An investigation at transonic speeds of the effects of thickness ratio and of thickened root sections on the aerodynamic characteristics of wings with 47° sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test section of the Langley 8-foot high-speed tunnel, by Ralph P. Bielat et al.

Title:	An investigation at transonic speeds of the effects of thickness ratio and of thickened root sections on the aerodynamic characteristics of wings with 47° sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test section of the Langley 8-foot high-speed tunnel
Author:	Bielat, Ralph P.
Author:	Coppolino, Domenic A.
Author:	Harrison, Daniel E.
Author:	United States. National Advisory Committee for Aeronautics
Note:	National Advisory Committee for Aeronautics, 1951

Link:	page images at HathiTrust
No stable link:	This is an uncurated book entry from our extended bookshelves, readable online now but without a stable link here. You should not bookmark this page, but you can request that we add this book to our curated collection, which has stable links.

Subject:	Aerodynamics, Transonic
Subject:	Airplanes -- Fuselage
Subject:	Airplanes -- Wings, Swept-back
Subject:	Charts, diagrams, etc.
Subject:	Drag (Aerodynamics)
Subject:	Fuselages
Subject:	Lift (Aerodynamics)
Subject:	Wind tunnel testing
Other copies:	Look for editions of this book at your library, or elsewhere.