Prediction of Flows about Forebodies at High-Angle-of-Attack Dynamic ConditionsA Reynolds-average Navier Stokes method developed for rotorcraft type of flow problems is applied for predicting the forces and moments of forebody models at high-angle-of-attack dynamic conditions and for providing insight into the flow characteristics at these conditions. Wind-tunnel results from rotary testing on generic forebody models conducted by NASA Langley and DERA are used for comparison. This paper focuses on the steady-state flow problem.
Document ID
20040040265
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
vanDam, C. P. (California Univ. Davis, CA, United States)
Saephan, S. (California Univ. Davis, CA, United States)
Fremaux, C. M. (NASA Langley Research Center Hampton, VA, United States)
DalBello, T. (Ohio Aerospace Inst. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2003
Publication Information
Publication: Symposium on Advanced Flow Management. Part A: Vortex Flows and High Angle of Attack for Military Vehicles. Part B: Heat Transfer and Cooling in Propulsion and Power Systems