Heat Transfer and Flow Characteristics Over a Lenticular Aerodynamic Body

Autor:	Kenneth J. Schneider, Harvey Dershin
Rok vydání:	1962
Předmět:	Materials science Angle of attack General Medicine Aerodynamics Mechanics Static pressure Heat transfer coefficient symbols.namesake Classical mechanics Mach number Drag Heat transfer symbols Oblique shock
Zdroj:	ARS Journal. 32:1269-1272
ISSN:	1936-9972
DOI:	10.2514/8.6262
Popis:	Experimental heat transfer and pressure distributions have been obtained, at a Mach number of 3.97, for the forward portion of a low drag lenticular aerodynamic body at zero angle of attack. It is shown that the experimental results can be predicted within engineering accuracy by using a simple strip analysis. Further, an interesting similarity for both the heat transfer coefficients and static pressures has been observed in the region of investigation .
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::5296d74ae8b501b737552ad9aedee1d3 https://doi.org/10.2514/8.6262 Zobrazit plný text záznamu