Accession Number:

ADA801527

Title:

Notes on the Application of Airfoil Studies to Helicopter Rotor Design

Personal Author(s):

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC

Report Date:

1948-09-22

Abstract:

A discussion is presented of a number of the problems most frequently arising in helicopter design, in order to facilitate the application of miscellaneous airfoil data to the problems of the helicopter designer. A reference is included of published reports on airfoil section characteristics or their application, which experience has shown to be useful in connection with these helicopter problems.

Descriptive Note:

Research memo.

Pages:

0015

Identifiers:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

5.40MB