Comparison of Hotshot Tunnel Force, Pressure Heat-transfer and Shock Shape Data with Shock Tunnel Data

Comparison of Hotshot Tunnel Force, Pressure Heat-transfer and Shock Shape Data with Shock Tunnel Data
Author :
Publisher :
Total Pages : 40
Release :
ISBN-10 : UOM:39015104951416
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis Comparison of Hotshot Tunnel Force, Pressure Heat-transfer and Shock Shape Data with Shock Tunnel Data by : E. E. Edenfield

Download or read book Comparison of Hotshot Tunnel Force, Pressure Heat-transfer and Shock Shape Data with Shock Tunnel Data written by E. E. Edenfield and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Comparison is made of force, pressure, heat-transfer, and shock shape data from tests in the AEDC-VKF hotshot tunnels and in the Cornell Aeronautical Laboratory 48 Inch Shock Tunnel. Several cone models of varying bluntness were tested through an angle-of-attack range of 0 to 40 deg at each facility. Excellent agreement of the hotshot and the shock tunnel data is shown. (Author).


Comparison of Hotshot Tunnel Force, Pressure Heat-transfer and Shock Shape Data with Shock Tunnel Data Related Books

Comparison of Hotshot Tunnel Force, Pressure Heat-transfer and Shock Shape Data with Shock Tunnel Data
Language: en
Pages: 40
Authors: E. E. Edenfield
Categories: Cone
Type: BOOK - Published: 1964 - Publisher:

DOWNLOAD EBOOK

Comparison is made of force, pressure, heat-transfer, and shock shape data from tests in the AEDC-VKF hotshot tunnels and in the Cornell Aeronautical Laboratory
NASA Technical Note
Language: en
Pages: 416
Authors:
Categories:
Type: BOOK - Published: 1968 - Publisher:

DOWNLOAD EBOOK

Pressure Distributions and Aerodynamic Characteristics of 90 and 150 Blunted Cones in Nitrogen and Helium at Mach 20
Language: en
Pages: 42
Authors: Theodore R. Creel
Categories: Aerodynamic load
Type: BOOK - Published: 1968 - Publisher:

DOWNLOAD EBOOK

Scientific and Technical Aerospace Reports
Language: en
Pages: 974
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1972 - Publisher:

DOWNLOAD EBOOK

Comparisons of Free-flight and Wind Tunnel Data on Slender Cones
Language: en
Pages: 32
Authors: B. J. Griffith
Categories: Aerodynamics
Type: BOOK - Published: 1964 - Publisher:

DOWNLOAD EBOOK

High Mach number wind tunnel drag, lift, moment, and heat-transfer data from sting-mounted models are compared, with available free-flight data. The resulting c