Accession Number : AD0451469

Title :   SUPERSONIC FLOW ABOUT RIGHT CIRCULAR CONES AT ZERO YAW IN AIR AT THERMODYNAMIC EQUILIBRIUM, PART III. TABLES OF DATA, CONT.,

Corporate Author : PICATINNY ARSENAL DOVER NJ FELTMAN RESEARCH LABS

Personal Author(s) : Hudgins, Henry E., Jr.

Report Date : SEP 1964

Pagination or Media Count : 817

Abstract : This material is a continuation of Part II and presents the cone flow properties of air in chemical equilibrium for altitudes from 100,000 to 200,000 feet at cone angles of 2.5 to 50 degrees, and various Mach numbers from 3.0 to 40.0. Part II presents the cone properties for altitudes from sea level to 80,000 feet. Part I presents an analysis and correlation of this data. The Table of Symbols has been reproduced in this report for the convenience of the reader. (Author)

Descriptors :   (*CONICAL BODIES, SUPERSONIC FLOW), WIND TUNNEL MODELS, MODEL TESTS, AERODYNAMIC CHARACTERISTICS, SUPERSONIC CHARACTERISTICS, HYPERSONIC FLOW, HYPERSONIC CHARACTERISTICS, THERMODYNAMICS, ENTHALPY, ENTROPY, STAGNATION POINT, SHOCK WAVES, PRESSURE, TEMPERATURE, NOSE CONES, REENTRY VEHICLES.

Distribution Statement : APPROVED FOR PUBLIC RELEASE