Dynamics of a light aircraft in spin
This paper focuses mainly on the experimental and in-flight spin investigations for an executive light airplane, named I-23 and built in the Institute of Aviation (Warsaw, Poland). It is a single-engine, all composite, straight wing, retractable undercarriage, conventional configuration and flight c...
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| Veröffentlicht in: | Aircraft Engineering 2002-01, Vol.74 (3), p.237-251 |
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| container_end_page | 251 |
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| container_title | Aircraft Engineering |
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| creator | Goraj, Zdobys aw Baron, Alfred Kacprzyk, Jan |
| description | This paper focuses mainly on the experimental and in-flight spin investigations for an executive light airplane, named I-23 and built in the Institute of Aviation (Warsaw, Poland). It is a single-engine, all composite, straight wing, retractable undercarriage, conventional configuration and flight control system airplane. In-flight spin tests confirmed good rudder and elevator effectiveness for spin recovery in a wide range of positions of the center of gravity. A typical time history of a spin entry and the developed spin and recovery is shown as well. |
| doi_str_mv | 10.1108/00022660210427422 |
| format | Article |
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A typical time history of a spin entry and the developed spin and recovery is shown as well.</description><subject>Aerodynamics</subject><subject>Aerospace industry</subject><subject>Aircraft</subject><subject>Aircraft accidents & safety</subject><subject>Aviation</subject><subject>Design</subject><subject>Equations of motion</subject><subject>Experiments</subject><subject>Gravitation</subject><subject>Mathematical models</subject><issn>1748-8842</issn><issn>0002-2667</issn><issn>1758-4213</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2002</creationdate><recordtype>article</recordtype><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><sourceid>GNUQQ</sourceid><recordid>eNqNkT1PwzAQhi0EEqXwA9gihGAh4DvbsTOi8ilVYoHZchwbUuULOx3670lVJooo093wPKfT-xJyCvQagKobSilillEEylFyxD0yASlUyhHY_nrnKlWK4yE5inFBKWSCsgk5v1u1pqlsTDqfmKSu3j-GxFTBBuOHpGqT2FftMTnwpo7u5HtOydvD_evsKZ2_PD7Pbuep5ZINqSw4L0yROyiFtJhhqUxBQXgqmCgM5xax8GAUY5nnKheZ95aDRWOMpMKzKbnc3O1D97l0cdBNFa2ra9O6bhm15FyCkgJH8uJPkgkQOVewE0SFSimR7wYloIBcjODZD3DRLUM75qLHqKUUgq__gw1kQxdjcF73oWpMWGmgel2Y3ipsdOjGcY0Lpi7_pVz9rmyhui89-wLl05-v</recordid><startdate>20020101</startdate><enddate>20020101</enddate><creator>Goraj, Zdobys aw</creator><creator>Baron, Alfred</creator><creator>Kacprzyk, Jan</creator><general>MCB UP Ltd</general><general>Emerald Group Publishing Limited</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7RQ</scope><scope>7TB</scope><scope>7WY</scope><scope>7XB</scope><scope>8AF</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BEZIV</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>F28</scope><scope>FR3</scope><scope>GNUQQ</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>K6~</scope><scope>KB.</scope><scope>L.-</scope><scope>L6V</scope><scope>L7M</scope><scope>M0F</scope><scope>M1Q</scope><scope>M2P</scope><scope>M7S</scope><scope>P5Z</scope><scope>P62</scope><scope>PDBOC</scope><scope>PQBIZ</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PTHSS</scope><scope>Q9U</scope><scope>7TC</scope></search><sort><creationdate>20020101</creationdate><title>Dynamics of a light aircraft in spin</title><author>Goraj, Zdobys aw ; 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| fulltext | fulltext |
| identifier | ISSN: 1748-8842 |
| ispartof | Aircraft Engineering, 2002-01, Vol.74 (3), p.237-251 |
| issn | 1748-8842 0002-2667 1758-4213 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_744718752 |
| source | Emerald |
| subjects | Aerodynamics Aerospace industry Aircraft Aircraft accidents & safety Aviation Design Equations of motion Experiments Gravitation Mathematical models |
| title | Dynamics of a light aircraft in spin |
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