NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Corrections on the Thermometer Reading in an Air StreamA method is described for checking a correction formula, based partly on theoretical considerations, for adiabatic compression and friction in flight tests and determining the value of the constant. It is necessary to apply a threefold correction to each thermometer reading. They are a correction for adiabatic compression, friction and for time lag.
Document ID
19930094460
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Van Der Maas, H J
Wynia, S
Date Acquired
September 6, 2013
Publication Date
October 1, 1940
Report/Patent Number
NACA-TM-956
Accession Number
93R23380
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available