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UNT Libraries Government Documents Department
Serial/Series Title:
NACA Technical Notes
Collection:
Technical Report Archive and Image Library
X-ray instrumentation for density measurements in a supersonic flow field
Date: December 1, 1952
Creator: Dimeff, John
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc56587/
The zero-lift drag of a 60 degree delta-wing-body combination (AGARD model 2) obtained from free-flight tests between Mach numbers of 0.8 and 1.7
Date: April 1, 1954
Creator: Piland, Robert O
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc56898/
The zero-lift drag of a slender body of revolution (NACA RM-10 research model) as determined from tests in several wind tunnels and in flight at supersonic speeds
Date: April 1, 1953
Creator: Evans, Albert J
Description: Presents zero-lift drag data of an NACA RM-10 slender body of revolution with and without stabilizing fins attached. The results from several wind tunnels and in flight are compared. The results cover a Reynolds number range from about 1 time 10 to the 6th power to 40 times 10 to the 6th power for the flight models. The Mach numbers covered include 1.5 to 2.4 in the wind tunnels and 0.85 to 2.5 in flight.
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc56732/
The zero-lift wave drag of a particular family of unswept, tapered wings with linearly varying thickness ratio
Date: May 1, 1955
Creator: Henderson, Arthur, Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc57644/