Type of Document	Master's Thesis
Author	Arledge, Thomas K.
URN	etd-12052009-020129
Title	ACSYNT aerodynamic estimation :an examination and validation for use in conceptual design
Degree	Master of Science
Department	Aerospace Engineering
Advisory Committee	Advisor Name Title Mason, William H. Committee Chair Durham, Wayne C. Committee Member Jayaram, Sankar Committee Member
Keywords	Aerodynamics
Date of Defense	1993-05-27
Availability	restricted
Abstract The aerodynamic prediction methodology available in ACSYNT is examined through comparison with aircraft data for a variety of classes of configurations. The predictions are a synthesis of the best empirical procedures currently available. The present work presents selected results obtained from the comparison, and shows how the basic capability can be enhanced by user supplied adjustments to represent changes in technology levels when considering advanced aircraft designs. The predictions and basis for adjustments are described for a supersonic cruise vehicle, a large subsonic transport, a typical fighter, an attack aircraft, and a typical business jet.
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