Accession Number : AD0451469


Title :   Supersonic Flow about Right Circular Cones at Zero Yaw in Air at Thermodynamic Equilibrium. Part 3. Tables of Data, Continued


Descriptive Note : Technical Report


Corporate Author : PICATINNY ARSENAL DOVER United States


Personal Author(s) : Hudgins,Henry


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/451469.pdf


Report Date : 01 Sep 1964


Pagination or Media Count : 820


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.


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