Experimental Investigation of a Turbulent Boundary Layer at Mach 6, High Reynolds Numbers, and Zero Heat Transfer

Experimental Investigation of a Turbulent Boundary Layer at Mach 6, High Reynolds Numbers, and Zero Heat Transfer
Author: Jerry B. Adcock
Publisher:
Total Pages: 66
Release: 1965
Genre: Turbulent boundary layer
ISBN:


Download Experimental Investigation of a Turbulent Boundary Layer at Mach 6, High Reynolds Numbers, and Zero Heat Transfer Book in PDF, Epub and Kindle


Experimental Investigation of a Turbulent Boundary Layer at Mach 6, High Reynolds Numbers, and Zero Heat Transfer
Language: en
Pages: 66
Authors: Jerry B. Adcock
Categories: Turbulent boundary layer
Type: BOOK - Published: 1965 - Publisher:

GET EBOOK

Experimental Investigation of the Turbulent Boundary Layer at a Mach Number of 6 with Heat Transfer at High Reynolds Numbers
Language: en
Pages: 82
Authors: Richard D. Samuels
Categories: Skim friction (Aerodynamics)
Type: BOOK - Published: 1967 - Publisher:

GET EBOOK

Experimental Investigation of a Turbulent Boundary Layer at Mach 6, High Reynolds Numbers, and Zero Heat Transfer
Language: en
Pages: 58
NASA Technical Note
Language: en
Pages: 936
Authors:
Categories:
Type: BOOK - Published: 1974 - Publisher:

GET EBOOK

Experimental Laminar, Transitional, and Turbulent Boundary-layer Profiles on a Wedge at Local Mach Number 6.5 and Comparisons with Theory
Language: en
Pages: 66
Authors: Michael C. Fischer
Categories: Boundary layer
Type: BOOK - Published: 1971 - Publisher:

GET EBOOK

Wind tunnel investigation of laminar, transitional, and turbulent boundary layer profiles on wedge at hypersonic speed to confirm theoretical analysis.