Choking of a Subsonic Induction Tunnel by the Flow from an Induction Nozzle Page: 1 of 21
This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided to Digital Library by the UNT Libraries Government Documents Department.
The following text was automatically extracted from the image on this page using optical character recognition software:
/ i . 9
y 1 l l + T L-+. " L r L i
NATIONAL ADVISORY COMMITTEE
TECHNICAL NOTE 2730
CHOKING OF A SUBSONIC INDUCTION TUNNEL BY THE
FLOW FROM AN INDUCTION NOZZLE
By W. F. Lindsey
Langley Aeronautical Laboratory
Langley Field, Va.
Here’s what’s next.
This report can be searched. Note: Results may vary based on the legibility of text within the document.
Tools / Downloads
Get a copy of this page or view the extracted text.
Citing and Sharing
Basic information for referencing this web page. We also provide extended guidance on usage rights, references, copying or embedding.
Reference the current page of this Report.
Lindsey, W. F. Choking of a Subsonic Induction Tunnel by the Flow from an Induction Nozzle, report, July 1952; (digital.library.unt.edu/ark:/67531/metadc56171/m1/1/: accessed December 18, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.