<DOC>
<DOCNO>
1331
</DOCNO>
<TITLE>
calculated responses of a large sweptwing airplane
to continuous turbulence with flight-test comparisons .
</TITLE>
<AUTHOR>
bennett,f.v. and pratt,k.g.
</AUTHOR>
<BIBLIO>
nasa tr r.69, 1960.
</BIBLIO>
<TEXT>
  calculated responses of symmetrical
airplane motions, wing deformations,
and wing loads due to gusts are
shown to compare favorably with
available flight-test results .  these
calculated responses are based on
random-process theory, five degrees of
freedom, lifting-surface aerodynamics,
and one-dimensional vertical
turbulence .  the extent to which
various degrees of freedom contribute
to the responses is examined and
in this connection the relative effects
of static and dynamic aeroelasticity
are determined .
</TEXT>
</DOC>
