Publication Date:
2019-08-28
Description:
The pockets of separation originating on the leading edges are surrounded by vortex sheets. Their configuration and intensity were determined by four conditions with the JONES approximation, which is itself corrected by a simple logic. Field pressures and stresses were computed for different cases and are compared with test results (pure deltas, swallow tails, truncations, strakes, ducks, fuselage).
Keywords:
AERODYNAMICS
Type:
NASA-TM-75863
,
Symp. of Appl. Aerodynamics; Nov 13, 1979 - Nov 15, 1979; Lille; France
Format:
application/pdf
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