Accession Number:

AD0895236

Title:

Wind-Tunnel Investigation of the RS-9 Meteor at Mach Numbers 1.56, 1.87, 2.16, 2.48, and 2.87,

Descriptive Note:

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s):

• Clancy, Thomas M.

Report Date:

1952-07-17

Pagination or Media Count:

171.0

Abstract:

The results of an investigation in the 40 x 40 cm Aeroballistics Tunnel No. 1 to determine pitch, yaw, and rolling moment data for the RS-9 Meteor are presented in this report. Author

Descriptors:

• *AIR TO AIR MISSILES
• SUPERSONIC CHARACTERISTICS
• WIND TUNNEL MODELS
• CANARD CONFIGURATIONS
• PITCH(MOTION)
• ROLL
• YAW
• MOMENTS
• ANGLE OF ATTACK
• STABILITY
• CENTER OF GRAVITY
• DATA PROCESSING

Subject Categories:

• Guided Missile Dynamics, Configurations and Control Surfaces
• Air- and Space-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE