Experimental investigation of a transonic potential flow around a symmetric airfoil

Author:: Meier, G. E. A.
Published:: Dec 1, 1981.
Physical Description:: 1 electronic document
Additional Creators:: Hiller, W. J.

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Summary:

Experimental flow investigations on smooth airfoils were done using numerical solutions for transonic airfoil streaming with shockless supersonic range. The experimental flow reproduced essential sections of the theoretically computed frictionless solution. Agreement is better in the expansion part of the of the flow than in the compression part. The flow was nearly stationary in the entire velocity range investigated.

Other Subject(s):

AERODYNAMICS

Collection:

NASA Technical Reports Server (NTRS) Collection.

Note:

Document ID: 19820006184.
Accession ID: 82N14057.
NASA-TM-76676.
REPT-10/1971.

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