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

Distribution Statement:

APPROVED FOR PUBLIC RELEASE