Accession Number:

AD0653568

Title:

WIND TUNNEL TEST REPORT CONVENTIONAL MODEL. VOLUME 2. LOW SPEED PRESSURE AND HINGE MOMENTS

Descriptive Note:

Corporate Author:

GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT

Personal Author(s):

Report Date:

1964-01-01

Pagination or Media Count:

347.0

Abstract:

The report presents the results from wind tunnel tests of a one- eighth scale conventional model of the U. S. Army XV-5A Lift Fan Flight Research Aircraft. Volume II presents hinge moment coefficients and pressure data in plotted and tabular form with pertinent detail explanatory information. Pressure and hinge moment data were not recorded during the second phase of the low speed testing.

Descriptors:

• *RESEARCH AIRCRAFT
• *VERTICAL TAKEOFF AIRCRAFT
• AERODYNAMIC CONTROL SURFACES
• DUCTED FANS
• LIFT
• MODEL TESTS
• MOMENTS
• PRESSURE
• TABLES(DATA)
• WIND TUNNEL MODELS

Subject Categories:

• Aerodynamics
• VSTOL
• Research and Experimental Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE