AN ANALYSIS OF THE EFFECTS OF BOUNDARY-LAYER-CONTROL AND PROPELLER CONFIGURATION ON THE PERFORMANCE OF AN ASW TYPE AIRPLANE

Document Details

Document Type: Technical Report
Publication Date: Aug 01, 1954
Accession Number: AD0053510

Entities

People

Kenneth Razak

Organizations

Wichita State University

Tags

Communities of Interest

Air Platforms

DTIC Thesaurus Topics

Aircrafts
Airplanes
Boundaries
Boundary Layer
Boundary Layer Control
Fixed Wing Aircraft
Layers
Propellers