NACA-TN-1428

Notes and tables for use in the analysis of supersonic flow

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:14:52Z
date available	2017-09-04T15:14:52Z
date copyright	01/01/1947
date issued	1947
identifier other	MEPTYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/13749
description abstract	This paper is a compilation of formulas, tables, and curves that has been found to be very useful in the analysis of supersonic wind-tunnel data. The information has been compiled by members of the Ames 1- by 3-foot supersonic wind-tunnel section with the specific needs of supersonic wind-tunnel operation in mind. With one exception, all tables and curves contained herein have been computed for the value of y = 1.400. The one exception is the curves showing the characteristics of cones in supersonic flow. These curves were taken directly from the data of references 1 and 2 wherein a value of y = 1.405 was used in the calculations.
language	English
title	NACA-TN-1428	num
title	Notes and tables for use in the analysis of supersonic flow	en
type	standard
page	86
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1947
contenttype	fulltext