MIL-HDBK-244A 6 apr 90.pdf
MIL-HDBK-244A 6 apr 90.pdf
MIL-HDBK-244A 6 apr 90.pdf
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<strong>MIL</strong>-<strong>HDBK</strong>-<strong>244A</strong><br />
5.1.7.1.2 Store carriage and se~arationaerodynamics. The aerodynamic<br />
effects of the stores on the aircraft’s flying qualities during carriage and<br />
separationsmust be carefully analyzedfor all possible store combinations<br />
during the initial aircraft design phases. Some of the more general aerodynamic<br />
characteristicsaffected by stores carriage which should be investigated,<br />
but not limited to, are the following:<br />
(a) Stability with external store carriage.<br />
(b) Stability with internal store carriage.<br />
(c) Engine ingestionof missile’exhaustgases.<br />
(d) Store release transients.<br />
5.1.7.1.2.1 Stabilitv with external carriage. Location of external<br />
stores relative to the wing leading edge and horizontal tail can have a<br />
marked effect on longitudinal stability and buffet characteristics. In addition,<br />
increasing wing sweep decreases the longitudinal stability with wing<br />
mounted external stores. Generally, airplanes with wing sweep greater than<br />
30 degrees showthe greatest stability loss with external stores---<br />
5.1.7.1.2.2 Stabilitv with internal carriage. For aircraft designed for<br />
internal store carriage, opening of the bomb”baydoors, similar panels or<br />
trapeze extensions should not excessivelydegrade the airplane flying<br />
qualities. Flying qualities effects such as buffet characteristics,directional<br />
stability, and longitudinal stability should be investigatedwith the<br />
bomb bay doors open (both full and to intermediatepositions) and operating.<br />
,<br />
5.1.7.1.2.3 Enaine ingestion of missile exhaust. Aircraft engineingestion<br />
of missile exhaust plumes from rocket motors can cause engine flame-out<br />
or degraded performance. Often to minimize adverse aircraft engine.characteristics<br />
due to missile exhaust gas ingestion, engine thrust levels are<br />
momentarily reduced during the missile or rocket firing sequence and airplane<br />
trim changes may ensue.<br />
5.1.7.2 Optimizing carriage aerodynamics. When designing an aircraft,<br />
the effect of store carriage on aircraft performance mustbe minimized.<br />
A great variety of stores is available in many different carriage combinations.<br />
For example, certain store combinations can produce an incremental<br />
drag equal to or even greater than the basic drag of the clean aircraft, and<br />
therefore, it is crucial to consider their effects on aircraft . performance.<br />
5.1.7.2.1 Choosinq carriage class. The two major classes of store<br />
carriage are “internal” and “external”. There are important effects of each<br />
to be considered in aircraft design, the choice of either or both types depending<br />
on mission requirements. An analytical approach backed up by substantial<br />
experimental proof will lead to the best store arrangement for a<br />
given mission.<br />
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