Calculation of Pressures on Bodies at Low Angles of Attack in Supersonic Flow

F. R. DeJarnette; C. P. Ford; D. E. Young

doi:10.2514/3.57770

journal article Nov 01, 1980

Calculation of Pressures on Bodies at Low Angles of Attack in Supersonic Flow

F. R. DeJarnette C. P. Ford D. E. Young

Journal of Spacecraft and Rockets Vol. 17 No. 6 pp. 529-536 · American Institute of Aeronautics and Astronautics (AIAA)

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References

11

[1]

Moore F.G. (1977)

[2]

Jackson C.M., Jr. NASA TN (1968)

[3]

3Syvertson, C.A. and Dennis, D.H. "A Second-Order Shock-Expansion Method Applicable to Bodies of Revolution Near Zero Lift," NACA Report 1328, 1957.

[4]

10.21236/ada055846

[5]

DeJarnette F.R. (1978)

[6]

Morrison A.M. (1975)

[7]

7Hsieh, T. "Flowfield Study About a Hemispherical Cylinder in Transonic and Low Supersonic Mach Number Range," AIAA Paper 75-83,1975. 10.2514/6.1975-83

[8]

10.1017/s0001925900000366

[9]

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10.2514/3.4228

Metrics

13

Citations

11

References

Details

Published: Nov 01, 1980
Vol/Issue: 17(6)
Pages: 529-536

Authors

F

F. R. DeJarnette

North Carolina State University, Raleigh, N. C.

C

C. P. Ford

North Carolina State University, Raleigh, N. C.

D

D. E. Young

Naval Surface Weapons Center, Dahlgren, Va.

Cite This Article

F. R. DeJarnette, C. P. Ford, D. E. Young (1980). Calculation of Pressures on Bodies at Low Angles of Attack in Supersonic Flow. Journal of Spacecraft and Rockets, 17(6), 529-536. https://doi.org/10.2514/3.57770

Calculation of Pressures on Bodies at Low Angles of Attack in Supersonic Flow

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