Title page for ETD etd-09082012-040433


Type of Document Master's Thesis
Author Wells, William R.
URN etd-09082012-040433
Title The prediction of aerodynamic force and moment coefficients on elliptic cone bodies at both angle of attack and sideslip by use of Newtonian impact theory
Degree Master of Science
Department Aeronautical Engineering
Advisory Committee
Advisor Name Title
Hassan, Hassan A. Committee Chair
Truitt, Robert W. Committee Member
Keywords
  • Lift (Aerodynamics)
Date of Defense 1961-05-05
Availability restricted
Abstract

Newtonian theory was applied, in this analysis, to the elliptic cone segment at angles of attack and sideslip. Closed form expressions fer the aerodynamic coefficients and static stability derivatives were obtained. Expressions for the full and half conic bodies were given and approximate expressions were given for the half cone case. The circular cone results were obtained as a special case of the general results. Comparisons of the theoretical calculations with experimental results at hypersonic speeds were made of the aerodynamic coefficients and static derivatives for several conic segments. Generally, good agreement was observed for specified ranges of fineness ratios and angles of attack.

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