Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction, by Robert J. Shaw et al.

Title:	Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction
Author:	Shaw, Robert J.
Author:	Neumann, Harvey E.
Author:	Wasserbauer, Joseph F.
Author:	Lewis Research Center
Author:	United States. National Aeronautics and Space Administration
Note:	U.S. National Aeronautics and Space Administration ;, 1976

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 -- Jet propulsion
Subject:	Airplanes -- Turbojet engines -- Air intakes
Subject:	Boundary layer control
Subject:	Contraction
Subject:	Cowlings
Subject:	Full scale tests
Subject:	Inlet flow
Subject:	Multiphase flow
Subject:	Porous walls
Subject:	Pressure reduction
Subject:	Scoops
Subject:	TF-30 engine
Subject:	Turbofan engines
Other copies:	Look for editions of this book at your library, or elsewhere.