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

Mechanical & Aerospace Engineering

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

4 Scopus citations

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 - Aug 1975

All Science Journal Classification (ASJC) codes

Aerospace Engineering

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10.2514/3.44482

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@article{fa71a7e14994466782ca93e62db7482c,

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

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

year = "1975",

month = aug,

doi = "10.2514/3.44482",

language = "English (US)",

volume = "12",

pages = "683--685",

journal = "Journal of Aircraft",

issn = "0021-8669",

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

number = "8",

}

TY - JOUR

T1 - Effect of combined roll rate and sideslip angle on aircraft flight stability

AU - Stengel, Robert F.

PY - 1975/8

Y1 - 1975/8

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UR - https://www.scopus.com/pages/publications/0016538255#tab=citedBy

U2 - 10.2514/3.44482

DO - 10.2514/3.44482

M3 - Article

AN - SCOPUS:0016538255

SN - 0021-8669

VL - 12

SP - 683

EP - 685

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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