Wind-Tunnel Investigation at Low Speed of the Static Longitudinal and Lateral Stability Characteristics of a 1/9-Scale Powered Model of the Convair XFY-1 Vertically Rising Airplane (open access)

Wind-Tunnel Investigation at Low Speed of the Static Longitudinal and Lateral Stability Characteristics of a 1/9-Scale Powered Model of the Convair XFY-1 Vertically Rising Airplane

"An experimental investigation has been made in the Langley stability tunnel at low speed to determine the static longitudinal and lateral stability characteristics of a 1/9-scale powered model of the Convair XFY-1 vertically rising airplane. Effects of thrust coefficient were investigated for the complete model and for certain components of the model. Effects of control deflections and of propeller-blade angle were investigated briefly for the complete model" (p. 1).
Date: February 11, 1953
Creator: Queijo, M. J.; Wolhart, W. D. & Fletcher, H. S.
Object Type: Report
System: The UNT Digital Library
Flight Measurements of the Stability Characteristics of the Bell X-5 Research Airplane in Sideslips at 59 Degrees Sweepback (open access)

Flight Measurements of the Stability Characteristics of the Bell X-5 Research Airplane in Sideslips at 59 Degrees Sweepback

"Flight measurements of the stability characteristics of the Bell X-5 research airplane at 59 deg sweepback were made in steady sideslips at Mach numbers from 0.62 to 0.97 at altitudes ranging between 35,000 and 40,000 feet. The results showed that the apparent directional stability was positive and increased at Mach numbers above 0.90. The apparent effective dihedral was positive and high, increasing at Mach numbers above 0.75" (p. 1).
Date: February 11, 1953
Creator: Childs, Joan M.
Object Type: Report
System: The UNT Digital Library
Preliminary Results of Stability and Control Investigation of the Bell X-5 Research Airplane (open access)

Preliminary Results of Stability and Control Investigation of the Bell X-5 Research Airplane

"During the acceptance tests of the Bell X-5 airplane, measurements of the static stability and control characteristics and horizontal-tail loads were obtained by the NACA High-Speed Flight Research Station. The results of the stability and control measurements are presented in this paper. A change in sweep angle between 20 deg and 59 deg had a minor effect on the longitudinal trim, with a maximum change of about 2.5 deg in elevator deflection being required at a Mach number near 0.85; however, sweeping the wings produced a total stick-force change of about 40 pounds" (p. 1).
Date: February 11, 1953
Creator: Finch, Thomas W. & Briggs, Donald W.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: S-4 (open access)

Texas Attorney General Opinion: S-4

Document issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, John Ben Shepperd, regarding a legal question submitted for clarification: Constitutionality of the provision in Senate Bill 98, 53rd Legislature, authorizing Boards of Trustees of independent school districts to appoint tax assessor-collectors for a term of office not to exceed three years.
Date: February 11, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
The T3 (p, y) He4 Reaction (open access)

The T3 (p, y) He4 Reaction

The excitation function for the reaction T3 (p, y) He4 has been extended to proton energies of 7.3 Mev. No experimental evidence is found for a resonance in the reaction up to this energy of bombarding protons.
Date: February 11, 1953
Creator: Birge, Robert W. & Jungerman, John A.
Object Type: Report
System: The UNT Digital Library