An Approximate Method for Calculation of the Laminar Boundary Layer with Suction for Bodies of Arbitrary Shape Page: 1 of 86
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:
AN APPROXIMATE METHOD FOR CALCULATION OF THE
LAMINAR BOUNDARY LAYER WITH SUCTION FOR
BODIES OF ARBITRARY SHAPE
By H. Schlichtlng
Translation of 'Ein Naherungsverfahren zur Berechnung der
laminaren Grenzschicht mit Absaugung bei beliebiger KSrperform"
from Aerodynamisches Institut der Technischen Hochschule
Braunschweig, Bericht 43/13, June 1943
March 1949 k" .r
... . L 4 :
NATIONAL ADVISORY COMMITTEE
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.
Schlichting, H. An Approximate Method for Calculation of the Laminar Boundary Layer with Suction for Bodies of Arbitrary Shape, report, March 1, 1949; (digital.library.unt.edu/ark:/67531/metadc64833/m1/1/: accessed January 20, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.