Effect of combined roll rate and sideslip angle on aircraft flight stability

Robert F. Stengel

doi:10.2514/3.44482

Effect of combined roll rate and sideslip angle on aircraft flight stability

Robert F. Stengel

Research output: Contribution to journal › Article › peer-review

Original language	English (US)
Pages (from-to)	683-685
Number of pages	3
Journal	Journal of Aircraft
Volume	12
Issue number	8
DOIs	https://doi.org/10.2514/3.44482
State	Published - Jan 1 1975
Externally published	Yes

All Science Journal Classification (ASJC) codes

Aerospace Engineering

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10.2514/3.44482

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title = "Effect of combined roll rate and sideslip angle on aircraft flight stability",

author = "Stengel, {Robert F.}",

year = "1975",

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pages = "683--685",

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issn = "0021-8669",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

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JO - Journal of Aircraft

JF - Journal of Aircraft

IS - 8

ER -

Effect of combined roll rate and sideslip angle on aircraft flight stability

All Science Journal Classification (ASJC) codes

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