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Preliminary Investigation at a Mach Number of 1.9 and a Reynolds Number of 2,200,000 of Three Ailerons Applicable to the Bell XS-2 Airplane Design
Report presenting testing of a 42.7 degree sweptback tapered wing with three types of ailerons tested at a Mach number of 1.9 and a Reynolds number of 2,200,000; the wing geometry was similar to that of an XS-2 airplane. The purpose of the investigation was to determine the effectiveness of ailerons at these specified flight characteristics. Results regarding the aerodynamic characteristics of the wing are also provided.
Date:
May 25, 1948
Creator:
Sivells, James C. & Conner, D. William
System:
The UNT Digital Library
Preliminary Report on the Hydrolytic Behavior of Cerium (IV)
The following report analyzes the hydrolytic behavior of cerium and compares them with the actinides of uranium and plutonium.
Date:
May 25, 1948
Creator:
Kraus, K. A.; Holmberg, R. W. & Nelson, F.
System:
The UNT Digital Library
The Ratio of Amino Acid Nitrogen to Creatinine in the Urine as a Sensitive Test for Uranium Poisoning
Report discussing experiments that were performed to determine whether amino acids in urine could be used as a test of subtle uranium poisoning.
Date:
May 25, 1948
Creator:
Berke, Harry & Rothstein, A.
System:
The UNT Digital Library
Wind-Tunnel Investigation of the Low-Speed Stability and Control Characteristics of a Model With a Sweptback Vee Tail and a Sweptback Wing
Report presenting testing in the 300 mph tunnel of a model with a sweptback vee tail and a sweptback wing to determine its low-speed stability and control characteristics. The results are compared to testing with the same tail panel with zero dihedral on the same wing-fuselage combination. The longitudinal stability characteristics, downwash at the tail, longitudinal control characteristics, lateral stability characteristics, and rudder control characteristics are provided.
Date:
May 25, 1948
Creator:
Polhamus, Edward C.
System:
The UNT Digital Library