| Title: | NACA Wartime Reports. Series L. |
| Alternate title: | Wind tunnel investigation of control surface characteristics. 12 - Various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal balance |
| Author: | Hoggard, H. Page |
| Author: | Langley Aeronautical Laboratory |
| Author: | United States. National Advisory Committee for Aeronautics |
| Note: | National Advisory Committee for Aeronautics, 1943 |
| 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: | Aerofoils |
| Subject: | Airplanes -- Control surfaces |
| Subject: | Charts, diagrams, etc. |
| Subject: | Flaps (Airplanes) |
| Subject: | Hinge moments (Aerodynamics) |
| Subject: | Plates (Engineering) |
| Subject: | Wind tunnel testing |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
Help with reading books -- Report a bad link -- Suggest a new listing
Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials
Books -- News -- Features -- Archives -- The Inside Story
Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.