Author: Lannie D. Webb
Publisher:
ISBN:
Category : Air-speed indicators
Languages : en
Pages : 68
Book Description
Characteristics and Use of X-15 Air-data Sensors
Author: Lannie D. Webb
Publisher:
ISBN:
Category : Air-speed indicators
Languages : en
Pages : 68
Book Description
Publisher:
ISBN:
Category : Air-speed indicators
Languages : en
Pages : 68
Book Description
Characteristics and Use of X-15 Air-data Sensors
NASA Technical Note
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
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
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
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
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 472
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 472
Book Description
Scientific and Technical Aerospace Reports
A Selected Listing of NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 470
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 470
Book Description
Wind Tunnel Investigation of an All Flush Orifice Air Data System for a Large Subsonic Aircraft
Author: Terry J. Larson
Publisher:
ISBN:
Category : Air speed
Languages : en
Pages : 104
Book Description
Publisher:
ISBN:
Category : Air speed
Languages : en
Pages : 104
Book Description
U.S. Government Research & Development Reports
Flight-test Results from Two Total Temperature Probes for Air-data Measurements Up to 2014 ̊K (3625 ̊R)
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.
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.