Structure of the conical flowfield about external axial cornersA theoretical and experimental investigation of the flowfield about symmetrical and asymmetrical external axial corners formed by the juncture of swept compressive wedges is presented. A study is made of the nature of inviscid cross flow stagnation points and their dependence on certain flow parameters is derived. The importance of imposing the physically relevant boundary condition for numerical simulations is discussed. For the asymmetrical wedge configuration, the proper boundary condition along the axial corner is shown to be a conical analog of Prandtl-Meyer flow. Further insight into the flow structure is revealed by the experimental results.
Document ID
19780036751
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Salas, M. D. (NASA Langley Research Center High-Speed Aerodynamics Div., Hampton, Va., United States)
Daywitt, J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 78-59Report Number: AIAA PAPER 78-59
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Huntsville, AL
Start Date: January 16, 1978
End Date: January 18, 1978
Sponsors: American Institute of Aeronautics and Astronautics