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A theoretical investigation of the aerodynamics of wing-tail combinations performing time-dependent motions at supersonic speeds
Report presenting a theoretical investigation of the contribution of horizontal tails to the lift and pitching moment due to angle of attack, a constant rate of pitch, and a constant vertical acceleration. Methods for calculating the flow fields behind wings with constant vertical acceleration are developed.
Date:
May 1954
Creator:
Martin, John C.; Diederich, Margaret S. & Bobbitt, Percy J.
System:
The UNT Digital Library
Stability derivatives of triangular wings at supersonic speeds
Report presenting the analysis of the stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds, which is extended to apply to triangular wings having large vertex angles and traveling at supersonic speeds.
Date:
May 1948
Creator:
Ribner, Herbert S. & Malvestuto, Frank S., Jr.
System:
The UNT Digital Library
An Analysis of the Factors Affecting the State of Fuel and Air Mixtures
From Introduction: "It is the purpose of this paper to describe the physical properties that are necessary to specify mixture quality in a system containing fuel and dry air and to evaluate the theoretical rolation between these properties and the physical properties of the mixture."
Date:
May 1946
Creator:
Gilbert, Mitchell; Howard, John N. & Hicks, Bruce L.
System:
The UNT Digital Library