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Full-scale wind tunnel-investigation of the Advanced Technology Light Twin-Engine airplane (ATLIT) (1980)

Hassell, J. L., Jr. ; Newsom, W. A., Jr. ; Yip, L. P.

In: CASI

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Publication Date: 2019-06-27

Description: An investigation was conducted to evaluate the aerodynamic performance, stability, and control characteristics of the Advanced Technology Light Twin Engine airplane (ATLIT). Data were measured over an angle of attack range from -4 deg to 20 deg for various angles of sideslip between -5 deg and 15 deg at Reynolds numbers of 0.0000023 and 0.0000035 for various settings of power and flap deflection. Measurements were also made by means of special thrust torque balances to determine the installed propeller characteristics. Part of the investigation was devoted to drag cleanup of the basic airplane and to the evaluation of the effect of winglets on drag and stability.

Keywords: AERODYNAMICS

Type: NASA-TP-1591 , L-13135

Format: application/pdf

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