Accession Number:
AD0647496
Title:
SUBSONIC WIND TUNNEL TESTS OF A .125 SCALE MODEL OF THE OV-10A AIRPLANE (ECP MODEL), VOLUME III.
Descriptive Note:
Technical rept.,
Corporate Author:
CORNELL AERONAUTICAL LAB INC BUFFALO N Y
Personal Author(s):
Report Date:
1966-08-01
Pagination or Media Count:
225.0
Abstract:
The report consists of test results presented in graphical form.
Subject Categories:
- Aerodynamics