During the past five years, under the support of the NASA Lewis Research Center, a research program related to aircraft and rotorcraft icing has been underway at Georgia Institute of Technology. The objectives of this effort are: (1) develop solution techniques capable of computing 3-D unsteady viscous flow past wing-alone and rotor configurations subjected to icing; and (2) assess the performance degradation in the aerodynamic characteristics of these configurations due to icing. Work carried out during the reporting period 1 Jan. - 30 Jun. 1991 is summarized.
Numerical investigation of performance degradation of wings and rotors due to icing
01.01.1991
Report
Keine Angabe
Englisch
Numerical Analysis of De-Icing Fluid Flow Off From Aircraft Wings
British Library Conference Proceedings | 2010
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