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Partner:
UNT Libraries Government Documents Department
Decade:
1950-1959
Serial/Series Title:
NACA Technical Notes
Collection:
National Advisory Committee for Aeronautics Collection
Boundary-layer Displacement Effects in Air at Mach Numbers of 6.8 and 9.6
Date: January 1, 1959
Creator: Bertram, M. H.
Description: Boundary layer displacement effects in air at mach 6.8 and 9.6.
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc52919/
An Analysis of Ramjet Engines Using Supersonic Combustion
Date: September 1, 1958
Creator: Weber, Richard J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc57482/
Analysis of the creep behavior of a square plate loaded in edge compression
Date: September 1, 1958
Creator: Mccomb, Harvey G , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc57275/
Analysis of turbulent flow and heat transfer in noncircular passages
Date: September 1, 1958
Creator: Deissler, Robert G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc57477/
Analytical and experimental investigation of temperature recovery factors for fully developed flow of air in a tube
Date: September 1, 1958
Creator: Weiland, W F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc57525/
An analytical study of turbulent and molecular mixing in rocket combustion
Date: September 1, 1958
Creator: Bittker, David A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc57133/
An approach to the problem of estimating severe and repeated gust loads for missile operations
Date: September 1, 1958
Creator: Press, Harry
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc57350/
Approximate method for calculating motions in angles of attack and sideslip due to step pitching- and yawing-moment inputs during steady roll
Date: September 1, 1958
Creator: Moul, Martin T
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc57209/
Approximate method for calculation of laminar boundary layer with heat transfer on a cone at large angle of attack in supersonic flow
Date: September 1, 1958
Creator: Brunk, William E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc57536/
Approximate solutions of a class of similarity equations for three-dimensional, laminar, incompressible boundary-layer flows
Date: September 1, 1958
Creator: Hansen, Arthur G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc57519/