Dynamic stability derivatives of a twin-jet fighter model for angles of attack from -10 ̊to 110
Sue B. Grafton and Charles E. Libbey.

APA Citation

Grafton, S. B., Libbey, C. E., Langley Research Center., United States. National Aeronautics and Space Administration. (1971). Dynamic stability derivatives of a twin-jet fighter model for angles of attack from -10 ̊to 110. Washington, D.C.: National Aeronautics and Space Administration .

MLA Citation

Grafton, Sue B, Charles E Libbey, Langley Research Center, and United States. National Aeronautics and Space Administration. Dynamic Stability Derivatives of a Twin-jet Fighter Model for Angles of Attack From -10 ̊to 110. Washington, D.C.: National Aeronautics and Space Administration , 1971.

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