Prediction of pressure distributions on axisymmetric bodies in transonic flow

Author:

YAROS S.1

Affiliation:

1. ARO, Inc., Arnold Air Force Station, Tenn.

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. ' x x x c d i n g s or the propulsion Intcrnctions IVorkshOp licld n t Langley Research Ccntrr, Ikmpton, VA 2 x 6 5 , hixy 19-20, 1976, SPonsorrd by thc lroplllsionAercdynnmics n l . n C h ,High-Speed Aerodynamics Division, &hi 1stop189. I+.II."Numerical cnlculntion of 'mansonic Boattail Flow," NASA TX D-79S4, June 1975.

2. 'Galighcr, L. L . , Yaros, S. F . , and Baucr, R. C."Evaluation of Boattail Geometry and Esliaust Plume Temperature Effect.s on Nozzle Aftcrbody Drag a t Transonic Yach Numbers, '* AEDC-TFi-76-102 (ADA030852), October 1976.

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