{[ promptMessage ]}

Bookmark it

{[ promptMessage ]}

spl7c - Test rig Force balance in 1 × 1 wind tunnel Drag...

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
Plain Vanilla Fuselage Drag Measurements 23 Mar 06 Lab 7 Lecture Notes C Plane Vanilla Drag Test Results Test article: Plane Vanilla fuselage, prop off.
Background image of page 1
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: Test rig: Force balance in 1 × 1 wind tunnel. Drag results: q ∞ (Pa) D (N) 5.47 0.0211 11.06 0.0411 20.79 0.0877 31.46 0.1243 1...
View Full Document

{[ snackBarMessage ]}