|
Abstract:
A program was conducted to assess materials and develop fabrication techniques for use in the manufacture of wing surface materials compatible with the application of laminar flow control to subsonic transport aircraft. Materials investigated included both aluminum alloys and nonmetallic composites. The concepts investigated included perforations and slots in the metallic test panels and microporosity and perforations in the composite test panels. (Author, modified).
| Description: |
Final Rept., Apr - Sep 76 |
| Pages: |
91 |
| Report Date: |
FEB 1977 |
| Contract Number: |
NAS114409 |
| Report Number: |
D699224 |
Report Unavailable |
| This title is unavailable from Storming Media. We do not know when it might be available, if at all. We list the report on our site for bibliographic completeness, to help our users know what other work has been performed in this field. Please note that as with all titles on this site, we do not have contact information for any of the authors. Nor can we give any suggestions on how one might obtain this report. |
|
|
|
Email This Abstract
