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Measurement of Static Forces on Internally Carried Bombs of Three Fineness Ratios in Flow Field of a Swept-wing Fighter-bomber Configuration at a Mach Number of 1.61 with Illustrative Drop Path CalculationsNo abstract available
Document ID
19700072759
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Carlson, H. W. (NASA Langley Research Center Hampton, VA, United States)
Smith, N. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 5, 2013
Publication Date
January 10, 1957
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L56I18
Report Number: NACA-RM-L56I18
Accession Number
70N72461
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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