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UNT Libraries Government Documents Department
Year:
1954
Month:
August
Performance of a 16-inch ram-jet engine with a can-type combustor at Mach numbers of 1.5 to 2.16
Date: August 27, 1954
Creator: Hearth, Donald P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc60637/
Aerodynamic characteristics at Mach number of 2.01 of two cruciform missile configurations having 70 degree delta wings with length-diameter ratios of 14.8 and 17.7 with several canard controls
Date: August 30, 1954
Creator: Spearman, M Leroy
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc60740/
Effects of canopy, revised vertical tail, and a yaw-damper vane on the aerodynamic characteristics of a 1/16-scale model of the Douglas D-558-II research airplane at a Mach number of 2.01
Date: August 30, 1954
Creator: Robinson, Ross B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc60649/
A flight evaluation of the stability and control of the X-4 swept-wing semitailless airplane
Date: August 30, 1954
Creator: Sadoff, Melvin
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc60733/
Pressure distributions on plug-and semaphore-type spoiler ailerons on a 35 degree sweptback wing of aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section at high subsonic speeds
Date: August 30, 1954
Creator: Hammond, Alexander D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc60410/