NASA Logo, External Link
Facebook icon, External Link to NASA STI page on Facebook Twitter icon, External Link to NASA STI on Twitter YouTube icon, External Link to NASA STI Channel on YouTube RSS icon, External Link to New NASA STI RSS Feed AddThis share icon
 

Record Details

Record 1 of 19462
Further Studies Of Hot-Wire Anemometry
Author and Affiliation:
Mckenzie, Robert(NASA Ames Research Center, Moffett Field, CA.)
Logan, Pamela(Stanford Univ.)
Bershader, Daniel(Stanford Univ.)
Abstract: Report discusses factors affecting readings of hot-wire anemometer in turbulent supersonic boundary layer. Represents extension of work described in "Hot-Wire Anemometry Versus Laser-Induced Fluorescence" (ARC-11802). Presents theoretical analysis of responses of hot-wire probe to changes in flow; also compares measurements by hot-wire probe with measurements of same flows by laser-induced fluorescence (LIF).
Publication Date: Dec 01, 1990
Document ID:
19900000629
(Acquired Nov 04, 1995)
Accession Number: 90B10629
Subject Category: PHYSICAL SCIENCES
Report/Patent Number: ARC-12104
Document Type: NASA Tech Brief
Publication Information: NASA Tech Briefs (ISSN 0145-319X); 14; 12; P. 31
Publisher Information: United States
Financial Sponsor: NASA; United States
Organization Source: NASA Ames Research Center; Moffett Field, CA, United States
Description: In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: HOT-WIRE ANEMOMETERS; SUPERSONIC BOUNDARY LAYERS; TURBULENT BOUNDARY LAYER
Availability Source: National Technology Transfer Center (NTTC), Wheeling, WV
Availability Notes: Additional information available through: National Technology Transfer Center (NTTC), Wheeling, WV 26003, (Tel: 1-800-678-6882).
› Back to Top
Find Similar Records
NASA Logo, External Link
NASA Official: Gerald Steeman
Site Curator: STI Program
Last Modified: August 18, 2011
Contact Us