000003362 001__ 3362
000003362 005__ 20141118153402.0
000003362 04107 $$acze
000003362 046__ $$k2005-05-09
000003362 100__ $$aSalga, J.
000003362 24500 $$aAirplane level turn at regimes of thrust deficit

000003362 24630 $$n11.$$pENGINEERING MECHANICS 2005
000003362 260__ $$bInstitute of Thermomechanics AS CR, v.v.i., Brno
000003362 506__ $$arestricted
000003362 520__ $$2eng$$aIn this paper relations of a time deceleration an unsteady horizontal banked turn and corresponding flight direction change are derived. Time and angle are considered from the beginning of the turn up to the deceleration to the minimum speed. Turn is performed at such load factor when required thrust exceeds available one a thrust deficit causes airplane deceleration. Solution in dimensionless shape is based on analytical integration of the motion equations for airplane as mass point. Engine characteristics are expressed by available thrust constant with speed. Aerodynamic characteristics are expressed by parabolic polar curve limited by maximum value of the lift coefficient. Formulas are completed due generalizing diagrams to calculations make easier.

000003362 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000003362 653__ $$a

000003362 7112_ $$aENGINEERING MECHANICS 2005$$cSvratka (CZ)$$d2005-05-09 / 2005-05-12$$gEM2005
000003362 720__ $$aSalga, J.
000003362 8560_ $$ffischerc@itam.cas.cz
000003362 8564_ $$s867733$$uhttps://invenio.itam.cas.cz/record/3362/files/Salga-PT.pdf$$y
             Original version of the author's contribution as presented on CD, .
            
000003362 962__ $$r3238
000003362 980__ $$aPAPER