NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Longitudinal aerodynamic characteristics of two blunted cone reentry configurations at Mach numbers from 17.6 to 22.2 including some Reynolds number effectsLongitudinal aerodynamic characteristics of blunted cone reentry vehicle configurations at high Mach numbers, including Reynolds number effect
Document ID
19660010304
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Maddalon, D. V. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3320
Report Number: NASA-TN-D-3320
Accession Number
66N19593
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
BLUNT BODY
REENTRY VEHICLE
MACH NUMBER
REYNOLDS NUMBER EFFECT

Related Records

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