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Theoretical and experimental investigation of additive dragThe significance of additive drag is discussed and equations for determining its approximate value are derived. Charts are presented giving values of additive drag for open-nose inlets and for annular-nose inlets with conical flow at the inlet. The effects of variable inlet total-pressure recovery and static pressures on the center body are investigated, and an analytical method of predicting the variation of pressure on the center body with mass-flow ratio is given. Experimental values of additive drag are compared with values predicted by the methods.
Document ID
19930086494
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sibulkin, Merwin
Date Acquired
August 16, 2013
Publication Date
May 21, 1951
Report/Patent Number
NACA-RM-E51B13
Report Number: NACA-RM-E51B13
Accession Number
93R15784
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIR INLETS
AIRPLANES -PERFORMANCE
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