"'- :51 ~
The tub巴 opening in Fig. 3 is normal to the direction of
flight and at the leading edge. This opening will ram
directly into the undisturbed air ahead and register the aCtual
pressure the leading edge is act叫ly sub}巳ctedto during :'{he
Super sonic flight. At this speed any solid would be
'disinte-grated by the impact, but the air of being compressibleis
being compressed. Violent compression generateviolent heat,
j
tthis is how we get the lligh tG阿巴ra E'ure 0泣 I.he leadingι dge of a super SOn叫IC al
…
叫 H川川川…t叫叫心叫f缸趴圳圳itt刊i,this situation better than compression.
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FRONT VIEW FRoNT VIE\-I\
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r可After all, the soundness of any theory can only be
determinded by an actual test. It is not difficult to conduct
a test as described in Fig. 3. Today, most aircraft manufact-urers have the facility to conduct such test. However, a itest
in a· supersonic tunnel may not be proper in this case
,
Because the air n super sonic tunnel or tube is already
highlycompressed, to test the effect of compression maybe
erroneous.
Compression is not only responsible for this heat
phenomenon, it is also responsible for some very important
discovery as well as puzzling phenomena of this age.τh申 p
most eminent of them all is the ignition ·of an atomic bomb. It.was responsible by compression
,
they called it implosiol1.Thepuzzling phenomenon of ice crystal shroud found after an atomic explosion is no other thanthe trick of compression. Again it is a case of compression in open space.
Ifιany further explaination is needed I will be very glao
to furnish.
