Aero-engine and foil type infrared surface source bait combined radiation characteristic test method
A technology for aero-engine and radiation characteristics, which is applied in the field of infrared radiation characteristics testing, can solve the problems of low measurement accuracy, large errors, and no consideration of the influence of aero-engine mid-wave and long-wave reflected environmental radiation on measurement results, etc., to achieve improved Ability, the effect of accurate test results
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[0030] The technical solutions of the present invention will be clearly and completely described below in conjunction with the embodiments. Apparently, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0031] Such as Figure 1-2 As shown, the test method for the combined radiation characteristics of an aero-engine and a foil-type infrared surface source decoy includes the following steps:
[0032] Step 1: Set the working state of the aeroengine, the working state is the exhaust temperature of the aeroengine, and the exhaust temperature includes 770K and 970K;
[0033] Step 2: Set the launch state of the decoy bomb, which is launched statically from the ground, and the launch state is initial velocity and pitch angle...
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