Unsteady Transonic Flow Past Airfoils in Rigid Body Motion
Unsteady Transonic Flow Past Airfoils in Rigid Body Motion
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In our eReader you can find the full English version of the book. Read Unsteady Transonic Flow Past Airfoils in Rigid Body Motion Online - link to read the book on full screen. Our eReader also allows you to upload and read Pdf, Txt, ePub and fb2 books. In the Mini eReder on the page below you can quickly view all pages of the book - Read Book Unsteady Transonic Flow Past Airfoils in Rigid Body Motion
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And 2. And should be increased towards 2. As the mesh is refined. P20 The supersonic relaxation factor for the reduced potential in the steady routine. It is not greater than 1. And normally set to 1. P30 The relaxation factor for the circulation. It is usually set to 1. But can be increased PlOl P102 The increments of PlO as the mesh system is refined P103 1 time, 2 times and 3 times, respectively, Title Card 5 FRFORA j^j^pi^- The frequency rate (rad/time) and amplitude (degree) of the sinusoi...dal variation of angle of attack (in degrees) .
FREORM AMPLM The frequency rate and amplitude (mach number) of the sinusoidal variation of flight speed in mach number.
FREQRC AMPLC The frequency rate and amplitude of the sinusoidal variation of flight angle in degrees.
142 PERIOD The complete sinusoidal periods to be calculated. DEGREE The degree interval to plot the graphs, pressure distribution, the loading and the supersonic zone over the airfoil.
Title Card 6 ALPHAl The angle of attack in degrees.
What to read after Unsteady Transonic Flow Past Airfoils in Rigid Body Motion?
You can find similar books in the "Read Also" column, or choose other free books by I Chung Chang to read onlineMoreLess
To quickly assess the difficulty of the text, read a short excerpt:
And 2. And should be increased towards 2. As the mesh is refined. P20 The supersonic relaxation factor for the reduced potential in the steady routine. It is not greater than 1. And normally set to 1. P30 The relaxation factor for the circulation. It is usually set to 1. But can be increased PlOl P102 The increments of PlO as the mesh system is refined P103 1 time, 2 times and 3 times, respectively, Title Card 5 FRFORA j^j^pi^- The frequency rate (rad/time) and amplitude (degree) of the sinusoi...dal variation of angle of attack (in degrees) .
FREORM AMPLM The frequency rate and amplitude (mach number) of the sinusoidal variation of flight speed in mach number.
FREQRC AMPLC The frequency rate and amplitude of the sinusoidal variation of flight angle in degrees.
142 PERIOD The complete sinusoidal periods to be calculated. DEGREE The degree interval to plot the graphs, pressure distribution, the loading and the supersonic zone over the airfoil.
Title Card 6 ALPHAl The angle of attack in degrees.
What to read after Unsteady Transonic Flow Past Airfoils in Rigid Body Motion?
You can find similar books in the "Read Also" column, or choose other free books by I Chung Chang to read onlineMoreLess
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