NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Wind tunnel model and methodThe design and development of a wind tunnel model equipped with pressure measuring devices are discussed. The pressure measuring orifices are integrally constructed in the wind tunnel model and do not contribute to distortions of the aerodynamic surface. The construction of a typical model is described and a drawing of the device is included.
Document ID
19740009842
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Jackson, C. M., Jr. (NASA Langley Research Center Hampton, VA, United States)
Summerfield, D. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
February 12, 1974
Subject Category
Electronic Equipment
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-263815
Patent Number: US-PATENT-3,791,207
Patent Number: NASA-CASE-LAR-10812-1
Accession Number
74N17955
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-3,791,207|NASA-CASE-LAR-10812-1
Patent Application
US-PATENT-APPL-SN-263815

Related Records

IDRelationTitleN72-27272Superseded By
No Preview Available