Available Indexes

Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 /
by Charles B. Rumsey and Dorothy B. Lee.

Description

Tools

Main Author: Rumsey, Charles B.
Related Names: Lee, Dorothy B.
Language(s): English
Published: Washington D.C. : National Aeronautics and Space Administration, 1959.
Subjects: Transonic wind tunnels > Transonic wind tunnels / Testing.
Fighter planes > Fighter planes / Testing.
Aerodynamics, Supersonic > Aerodynamics, Supersonic / Testing.
Airplanes > Airplanes / Models > Airplanes / Models / Propellers > Airplanes / Models / Propellers / Testing.
Heat > Heat / Transmission > Heat / Transmission / Testing.
Note: "November 1959."
Cover title.
Full text also available online. Address as of 11/5/2010:
Physical Description: 47 p. : ill. ; 26 cm.
Locate a Print Version: Find in a library

Viewability

Item Link Original Source
Full view University of Illinois at Urbana-Champaign
View HathiTrust MARC record