Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7 - Info and Reading Options
By Don E. Avery
"Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7" was published by National Aeronautics and Space Administration, Scientific and Technical Information Branch in 1985 - Washington, D.C and the language of the book is English.
“Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7” Metadata:
- Title: ➤ Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7
- Author: Don E. Avery
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: Washington, D.C
“Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7” Subjects and Themes:
- Subjects: ➤ Cold surfaces - Heat shielding - Hypersonic flow - Impingement - Reusable heat shielding - Thermal protection - Tiles - Turbulent boundary layer - Turbulent flow
Edition Specifications:
- Format: Microform
- Pagination: 1 v.
Edition Identifiers:
- The Open Library ID: OL17724417M - OL7275331W
AI-generated Review of “Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7”:
Read “Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7”:
Read “Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7” by choosing from the options below.
Search for “Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7” downloads:
Visit our Downloads Search page to see if downloads are available.
Find “Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7” in Libraries Near You:
Read or borrow “Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7” from your local library.
Buy “Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7” online:
Shop for “Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7” on popular online marketplaces.
- Ebay: New and used books.