Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80° delta-wing missile, by Eugene D. Schult et al.

Title:	Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80° delta-wing missile
Author:	Schult, Eugene D.
Author:	Langley Research Center
Note:	National Aeronautics and Space Administration, 1960

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:	Control surfaces
Subject:	Delta wings
Subject:	Drag
Subject:	Free flight
Subject:	Jet control
Subject:	Mach number
Subject:	Spanwise blowing
Subject:	Spoilers
Subject:	Subsonic speed
Subject:	Thrust control
Subject:	Trailing edges
Subject:	Wakes
Subject:	Wedge flow
Subject:	Zero lift
Other copies:	Look for editions of this book at your library, or elsewhere.