NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Wind-tunnel Investigation of a High-critical-speed Fuselage Scoop Including the Effects of Boundary Layer
Document ID
19930092959
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Baals, Donald D
Date Acquired
September 6, 2013
Publication Date
February 1, 1945
Report/Patent Number
NACA-ACR-L5B01A
NACA-WR-L-733
Report Number: NACA-ACR-L5B01A
Report Number: NACA-WR-L-733
Accession Number
93R22249
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SCOOPS
PRESSURE DISTRIBUTION - FUSELAGES
WIND TUNNEL TESTS - NACA - HIGH-SPEED (8')
BOUNDARY LAYER
PHOTOGRAPHY - AIR FLOW - SCOOPS - TUFTS
MACH NUMBER

Related Records

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