Accession Number:

ADA801516

Title:

The Relation between Spanwise Variations in the Critical Mach Number and Spanwise Load Distributions

Personal Author(s):

Corporate Author:

NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS LANGLEY FIELD VA LANGLEY AERONAUTICAL LABORATORY

Report Date:

1944-12-01

Abstract:

Data are presented to show the changes that occur in the spanwise load distributions on wings when the critical Mach number is exceeded. These data indicate that the magnitude of the changes in spanwise load distribution varies with the magnitude of the spanwise variation in the critical Mach numbers of the sections. Means of reducing the magnitudes of such changes are considered.

Descriptive Note:

Wartime rept.

Pages:

0012

Identifiers:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

1.13MB