Accession Number:

AD0768420

Title:

The Effect of Airplane Propeller on a Tunnel-Type Sprayer,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Logachev,Yu. G.
• Baryshev,E. S.

Report Date:

1973-10-01

Pagination or Media Count:

18.0

Abstract:

When the parameters of tunnel-type sprayers are calculated and selected, it is necessary to take into consideration the effect of the plane on the air streamlining of these sprayers. On a plane the greatest influence usually comes from the propeller. The report presents the results of experimental studies of this effect.

Descriptors:

• *SPRAYS
• *AERIAL PROPELLERS
• FLUID DYNAMICS
• SPRAY NOZZLES
• ANGLE OF ATTACK
• WIND TUNNEL MODELS
• STAGNATION POINT
• FLUID FLOW
• USSR

Subject Categories:

• Aerodynamics
• Aircraft
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE