Characteristics and Use of X-15 Air-data Sensors
Author: Lannie D. Webb
Publisher:
Published: 1968
Total Pages: 68
ISBN-13:
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Author: Lannie D. Webb
Publisher:
Published: 1968
Total Pages: 68
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. Superintendent of Documents
Publisher:
Published: 1968
Total Pages:
ISBN-13:
DOWNLOAD EBOOKFebruary 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:
Published: 1991
Total Pages: 1460
ISBN-13:
DOWNLOAD EBOOKLists 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: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Published:
Total Pages: 472
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
Published: 1969
Total Pages: 470
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1967
Total Pages: 204
ISBN-13:
DOWNLOAD EBOOKAuthor: Terry J. Larson
Publisher:
Published: 1980
Total Pages: 104
ISBN-13:
DOWNLOAD EBOOKAuthor: Jack Nugent
Publisher:
Published: 1972
Total Pages: 60
ISBN-13:
DOWNLOAD EBOOKAn 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:
Publisher:
Published: 1969
Total Pages: 840
ISBN-13:
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