Effects of plan form, airfoil section, and angle of attack on the pressures along the base of blunt-trailing-edge wings at Mach numbers of 1.41, 1.62, and 1.96 Page: 4 of 54

brightness
contrast
saturation
exposure
gamma
Applying filters

Upcoming Pages

Here’s what’s next.

upcoming item: 5 5 of 54
upcoming item: 6 6 of 54
upcoming item: 7 7 of 54
upcoming item: 8 8 of 54

Show all pages in this report.

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.

Goin, Kennith L. Effects of plan form, airfoil section, and angle of attack on the pressures along the base of blunt-trailing-edge wings at Mach numbers of 1.41, 1.62, and 1.96, report, September 16, 1952; (digital.library.unt.edu/ark:/67531/metadc59299/m1/4/: accessed December 14, 2017), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.