Accession Number:

AD0637698

Title:

HYPERSONIC STATIC STABILITY INVESTIGATION OF A TOMAHAWK 20-PERCENT-SCALE MODEL

Descriptive Note:

Corporate Author:

ARO INC ARNOLD AFS TN

Personal Author(s):

Report Date:

1966-08-01

Pagination or Media Count:

20.0

Abstract:

An experimental investigation was conducted to obtain detailed static stability, induced roll and yaw, and roll forcing information on several configuration of a Tomahawk 20-percent-scale model. Tests were conducted at nominal Mach numbers of 6 and 8, free-stream Reynolds numbers of 2,500,000 and 5,000,000 per foot, angles of attack from -2 to 14 deg, and roll angles from 0 to 90 deg. Selected results are presented to illustrate types and quality of data obtained.

Subject Categories:

  • Rockets

Distribution Statement:

APPROVED FOR PUBLIC RELEASE