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Mach did not see much hope, but he was ready to fight.
There seemed to be a play of force around Mach, but nothing else happened.
"Why did Mach put you into our power for help?"
There was no sign of him, but Mach could tell.
As he said, it was easy for Mach to check.
The speed of sound is also known as Mach 1.
They had to write her off, as Mach put it.
Mach knew that he was in for a difficult scene.
When Mach was first being seriously used in the 2.
Was it really too late to go back - to make her peace with Mach?
So Mach would have the magic through- out the game.
Test with speed up to Mach 20 where reached around 2001.
Mach looked at the packet a moment, then took one.
At Mach three or better it should be overhead soon.
Maybe even better than before, in fact, because this gave him a chance to work much closer with Mach.
Mach called again, making sure the rider could find him.
Mach took the comb and began working on her hair.
"Because you have no technology of your own," Mach said.
The missile was now moving toward him at Mach 1.5.
This research program suggested that Mach 25 might be possible.
Mach stood there a moment longer, looking up at the screen.
Tan did not like Mach, but had to work with him.
She turned back to Mach, and put her arms around him, drawing herself close.
"We were looking for a place to rest in safety," Mach said.
A running start of Mach 15 or so would be worthwhile.
The above equation is only for Mach numbers less than 1.0.
With heating, Mach numbers of up to 11 can be reached.
Mach number is given as a percentage compared to the local speed of sound.
More specifically, it is a flow whose Mach number exceeds 1.
The new intake also was designed to be more efficient at higher Mach numbers.
Or sound would, at that Mach numbers corresponding to those speeds, if it could?
A sign inside the cabin displays the Mach number continuously.
At altitude, for reasons explained, Mach number is a function of temperature.
If we use the Mach number equation for dry air:
They are a measure of rotor blade tip Mach number.
Consequently, the distance between the shock and the body decreases at higher Mach numbers.
This allows the mach number of an aircraft to be higher than that actually experienced by the wing.
The phenomena associated with problems at the critical Mach number became known as compressibility.
Mach numbers up to 4 are easily obtained without any additional heating of the flow.
Based on this, and prior studies, they concluded that the gas flows at a low Mach number (less than two).
Flow in this regime is still Mach number dependent.
Four tests took place, reaching Mach numbers of 5.5, 5.35, 5.8, and 6.5.
The speed brakes were not damaged and succeeded in reducing the Mach number.
Pressure waves build up on aircraft surfaces differently at different Mach numbers.
In general, this is the case where the Mach number in part or all of the flow exceeds 0.3.
No variation of density, speed of sound and Mach number is allowed.
The Kelvin scale, however, is used for Mach number calculations.
A Mach number is a number that describes speed.
The wing and tail thickness ratio was also reduced to increase the critical Mach number.
With falling flight Mach number, the cold nozzle pressure ratio decreases.