Elevator Hinge moment studies over generic winged body configuration
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Elevator Hinge moment studies over generic winged body configuration
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| Creator |
Rajan, Kurade
Sampath, Rao |
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| Subject |
Astrodynamics
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| Description |
Elevator hinge moment measurements have been carried out on a generic wing body configuration through wind tunnel
tests. Tests have been carried out at subsonic and transonic Mach numbers in the angles of attack range -4° to 24°. Maximum
hinge moment coefficient occurs in the transonic region as expected. Positive deflections of elevator produce higher elevator hinge moment coefficient compared to that of negative deflections. Elevator hinge moment coefficient is linear with elevator deflection up to ±10° and angles of attack up to 10°.
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| Date |
2011
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| Type |
Conference or Workshop Item
PeerReviewed |
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| Format |
application/pdf
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| Identifier |
http://nal-ir.nal.res.in/10113/1/256_G02_(1).pdf
Rajan, Kurade and Sampath, Rao (2011) Elevator Hinge moment studies over generic winged body configuration. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), 16-18 November 2011, Bangalore. |
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| Relation |
http://nal-ir.nal.res.in/10113/
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