NACA-RM-L53L28 REV A

Pressures and associated aerodynamic and load characteristics for two bodies of revolution at transonic speeds

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:09:42Z
date available	2017-09-04T15:09:42Z
date copyright	01/01/1954
date issued	1954
identifier other	APSWXDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/7835
description abstract	INTRODUCTION A detailed study of the pressures and resulting forces for a body of revolution, designated "curved body" in this report, at transonic speeds has been presented in reference 1. The present tests were undertaken in order to provide aerodynamic load data for a body of revolution having an ogive nose and cylindrical afterbody and to compare the aerodynamic characteristics of this body with the body of reference 1 at transonic speeds. The body used in the present test is designated "cylindrical body" herein. A comparison of various theoretical aerodynamic parameters with experimental values is included. The tests reported herein were made for a Mach number range from 0.6 to 1.13 and an angle-of-attack range from O^o t o 20°. Reynolds number range corresponding to the Mach number range varied from 3.3 x 10 ⁶ t o 3.9 x 10 ⁶ per foot of length.
language	English
title	NACA-RM-L53L28 REV A	num
title	Pressures and associated aerodynamic and load characteristics for two bodies of revolution at transonic speeds	en
type	standard
page	35
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1954
contenttype	fulltext