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Performance of Air Inlets at Transonic and Low Supersonic SpeedsA general discussion of the air-inlet problem is presented. Recently obtained drag and pressure-recovery data for transonic-type nose, scoop, and wing-root inlets are summarized. Preliminary results concerning the performance of the sharp-edged supersonic-type inlets at transonic and subsonic speeds also are given.
Document ID
19930086995
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Nichols, Mark R
Pendley, Robert E
Date Acquired
August 16, 2013
Publication Date
February 15, 1952
Report/Patent Number
NACA-RM-L52A07
Report Number: NACA-RM-L52A07
Accession Number
93R16285
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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