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Analysis of wind tunnel test results for a 9.39-per cent scale model of a VSTOL fighter/attack aircraft. Volume 3: Effects of configuration variations from baseline

J. R. Lummus, G. T. Joyce, C. D. Omalley

Abstract

The aerodynamic characteristics of the components of the baseline E205 configuration is presented. Geometric variations from the baseline E205 configuration are also given including a matrix of conrad longitudinal locations and strake shapes.

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Available abstract

Key concepts: Baseline (sea), Aerodynamics, Volume (thermodynamics), Wind tunnel, Scale (ratio), Scale model, Engineering, Aerospace engineering