Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers of 0.40 to 0.93 of a 45° sweptback wing of aspect ratio 4, by Kenneth P. Spreemann et al.

Title:	Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers of 0.40 to 0.93 of a 45° sweptback wing of aspect ratio 4
Author:	Spreemann, Kenneth P.
Author:	Alford, William J.
Author:	Langley Aeronautical Laboratory
Author:	United States. National Advisory Committee for Aeronautics
Note:	National Advisory Committee for Aeronautics, 1957

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:	Airplanes -- Fuselage
Subject:	Airplanes -- Wings, Swept-back
Subject:	Drag (Aerodynamics)
Subject:	Flaps (Airplanes)
Subject:	Fuselages
Subject:	Leading edge flaps
Subject:	Leading edges (Aerodynamics)
Subject:	Lift (Aerodynamics)
Subject:	Pitching (Aerodynamics)
Other copies:	Look for editions of this book at your library, or elsewhere.