ESDU 00025:2014
$126.75
Computer program for prediction of aircraft lateral stability derivatives in sideslip at subsonic speeds
| Published By | Publication Date | Number of Pages |
| ESDU | 2014-04-01 | 86 |
ESDU 00025 describes the construction of input files for the
computer program ESDUpac A0025, which combines and extends the
prediction methods of twenty five individual ESDU Data Items to
evaluate the lateral stability derivatives in an aerodynamic-body
axis system. The effect of under-wing pylon-mounted jet engine
nacelles or wing-mounted nacelles for propeller driven aircraft is
included. The deflection of up to four flap panels on each
half-wing is permitted. Worked examples illustrate the use of the
program.
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