Wind-tunnel investigation of the effects of various dorsal-fin and vertical-tail configurations on the directional stability of a streamlined body at transonic speeds, transonic-bump method, by Harold S. Johnson et al.

Title:	Wind-tunnel investigation of the effects of various dorsal-fin and vertical-tail configurations on the directional stability of a streamlined body at transonic speeds, transonic-bump method
Author:	Johnson, Harold S.
Author:	Hayes, William C.
Author:	Langley Aeronautical Laboratory
Author:	United States. National Advisory Committee for Aeronautics
Note:	Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953

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 -- Tail surfaces
Subject:	Stability of airplanes
Subject:	Wind tunnel testing
Other copies:	Look for editions of this book at your library, or elsewhere.