Flight-test Results from Two Total Temperature Probes for Air-data Measurements Up to 2014 ̊K (3625 ̊R) PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Flight-test Results from Two Total Temperature Probes for Air-data Measurements Up to 2014 ̊K (3625 ̊R) PDF full book. Access full book title Flight-test Results from Two Total Temperature Probes for Air-data Measurements Up to 2014 ̊K (3625 ̊R) by Jack Nugent. Download full books in PDF and EPUB format.
Author: Jack Nugent Publisher: ISBN: Category : Fluidic devices Languages : en Pages : 60
Book Description
An experimental temperature probe package containing a fluidic oscillator temperature probe and a shielded thermocouple temperature probe was tested during several X-15 flights. The X-15 flights provided greatly varying test conditions, including a wide range of rapidly changing total temperatures and Mach numbers which extended from subsonic to hypersonic speeds. Within restricted ranges of free-stream Mach number, free-stream unit weight flow, and local stagnation pressure, both probes yielded ramp outputs of temperature parallel to ramp inputs of free-stream total temperature. Within these ranges both probes were used to determine total temperature in the Mach 6 temperature environment. Because ambient temperature was known, both probes were used to estimate velocity and Mach number.
Author: Jack Nugent Publisher: ISBN: Category : Fluidic devices Languages : en Pages : 60
Book Description
An experimental temperature probe package containing a fluidic oscillator temperature probe and a shielded thermocouple temperature probe was tested during several X-15 flights. The X-15 flights provided greatly varying test conditions, including a wide range of rapidly changing total temperatures and Mach numbers which extended from subsonic to hypersonic speeds. Within restricted ranges of free-stream Mach number, free-stream unit weight flow, and local stagnation pressure, both probes yielded ramp outputs of temperature parallel to ramp inputs of free-stream total temperature. Within these ranges both probes were used to determine total temperature in the Mach 6 temperature environment. Because ambient temperature was known, both probes were used to estimate velocity and Mach number.
Author: United States. Superintendent of Documents Publisher: ISBN: Category : Government publications Languages : en Pages : 1194
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Author: Publisher: ISBN: Category : Aeronautics Languages : en Pages : 946
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: David F. Fisher Publisher: ISBN: Category : Transportation Languages : en Pages : 526
Book Description
A bibliography of Technical Reports from Dryden Research Center, 1946-1996. Dryden was a National Advisory Committee for Aeronautics (NACA) facility from to 1946-1958, when NACA became NASA (National Aeronautics and Space Administration). This bibliography encompasses both NACA and NASA publications. Illustrated with diagrams and photos. Black and white version.
Author: Jack Nugent
Author: Jack Nugent
Author: United States. Superintendent of Documents
Author: 
Author: 
Author: 
Author: United States. Superintendent of Documents
Author: 
Author: David F. Fisher
Author: 
Author: