Flight Performance of a Circulation Controlled STOL Aircraft

J.L. Loth; J.B. Fanucci; S.C. Roberts

doi:10.2514/3.58647

journal article Mar 01, 1976

Flight Performance of a Circulation Controlled STOL Aircraft

J.L. Loth J.B. Fanucci S.C. Roberts

Journal of Aircraft Vol. 13 No. 3 pp. 169-173 · American Institute of Aeronautics and Astronautics (AIAA)

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References

8

[1]

^avidson, I.M., Aerofoil Boundary-Layer Control System, British Patent No. 913754,1960.

[2]

10.1017/s0001925900004558

[3]

10.1017/s0001925900004613

[4]

Walters R.E. (1972)

[5]

Ambrosiani J.B. (1971)

[6]

Loth J.L. (1974)

[7]

Loth J.L. (1973)

[8]

10.2514/6.1974-502

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Metrics

39

Citations

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References

Details

Published: Mar 01, 1976
Vol/Issue: 13(3)
Pages: 169-173

Authors

J

J.L. Loth

West Virginia University, Morgantown, W. Va.

J

J.B. Fanucci

West Virginia University, Morgantown, W. Va.

S

S.C. Roberts

Flight Research, Inc., State College, Miss.

Cite This Article

J.L. Loth, J.B. Fanucci, S.C. Roberts (1976). Flight Performance of a Circulation Controlled STOL Aircraft. Journal of Aircraft, 13(3), 169-173. https://doi.org/10.2514/3.58647

Flight Performance of a Circulation Controlled STOL Aircraft

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