Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44

Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44
Author :
Publisher :
Total Pages : 26
Release :
ISBN-10 : NASA:31769000459241
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44 by :

Download or read book Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44 written by and published by . This book was released on 1959 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44 Related Books

Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44
Language: en
Pages: 26
Heat Transfer and Pressure Measurement on a 5-inch Hemispherical Concave Nose at a Mach Number of 2.0
Language: en
Pages: 24
Authors: J. Thomas Markley
Categories: Heat
Type: BOOK - Published: 1958 - Publisher:

GET EBOOK

Abstract: The concave-nose stagnation-point heating is 40 percent of that of a hemisphere nose shape having the same diameter. At angles of attack of ℗±5© a
Laminar Heat-transfer and Pressure-distribution Studies on a Series of Reentry Nose Shapes at a Mach Number of 19.4 in Helium
Language: en
Pages: 44
Authors: Richard D. Wagner
Categories: Fluid mechanics
Type: BOOK - Published: 1961 - Publisher:

GET EBOOK

Local Heat Transfer to Blunt Noses at High Supersonic Speeds
Language: en
Pages: 16
Authors: William E. Stoney
Categories: Aerodynamic heating
Type: BOOK - Published: 1957 - Publisher:

GET EBOOK

Heat-transfer and Pressure Measurements on Flat-faced Cylinders at a Mach Number of 2
Language: en
Pages: 38
Authors: William E. Stoney
Categories: Cylinders
Type: BOOK - Published: 1958 - Publisher:

GET EBOOK

Flat-faced cylinders of 12-inch dtameter and 4-inch diameter were tested at a Mach number of 2 and sea-level conditions in the preflight jet of the Langley Pilo