Rotor wake effects on hub/pylon flow
By: Paul Soohoo ... [et al.], Aerospace Systems, Inc. ; prepared for Applied Technology Laboratory, U.S. Army Research and Technology Laboratories (AVRADCOM).
Contributors: Soohoo, Paul.; Army Research and Technology Laboratories (U.S.). Applied Technology Laboratory.; Aerospace Systems Inc.
Series: USARTL-TR ; 78-1 A; USARTL-TR ; 78-1 B
Publisher: [Dept. of Defense, Dept. of the Army], Army Materiel Development and Readiness Command, Army Aviation Research and Development Command, Army Research and Technology Laboratories, Applied Technology Laboratory
Published: 1978
Place of publication: Fort Eustis, Va
Language: eng
Subjects: Wakes (Aerodynamics); Helicopters.
Notes: Final report for period June 1975--September 1977.

Contract no. DAAJ02-75-C-0041.

May 1978.

Includes bibliographical references.
Table of contents: value: v. 1. Theoretical formulation.; value: v. 2. Program SHAPES user's manual.