Accession Number:

AD0435470

Title:

EXPANSIVE FLOW TABLES PERTINENT TO JET FLOW CALCULATIONS

Descriptive Note:

Corporate Author:

ARO INC ARNOLD AFS TN

Personal Author(s):

• Lyons, S. C.

Report Date:

1964-04-01

Pagination or Media Count:

315.0

Abstract:

Charts and tables are presented for determining approximate values of the initial turning angles and the boundary shapes of jets exhausting to low ambient temperatures. The tables have been compiled to facilitate calculations pertaining to jet flow for various ratios of specific heats from 1.10 to 1.667 and Mach numbers from 1.0000 to 100.00. The ratios pp sub t and AA at the nozzle throat and the Prandtl-Meyer angle are given for each Mach number and ratio of specific heats.

Descriptors:

• *JET FLOW
• *EXHAUST GASES
• TABLES(DATA)
• ROCKET NOZZLES
• SPECIFIC HEAT
• HIGH ALTITUDE
• PRESSURE

Subject Categories:

• Fluid Mechanics
• Combustion and Ignition

Distribution Statement:

APPROVED FOR PUBLIC RELEASE