electricpete
Electrical
- May 4, 2001
- 16,774
Dunkerely's method tells us that if we have a system of discrete springs and masses, we can combine the resonant frequencies associated with each single mass alone attached to the system of springs using:
1/w^2 = 1/w1^2 + 1/w2^2 + ....
The only proof I have seen of Dunkerley's method uses discrete masses. But it seems that Dunkerely gives a good estimate of the natural frequency for several systems that include distributed mass (examples below). Does Dunkerley apply for systems that include distributed masses? Is the resulting calculated frequencies always a lower bound as it is when only discrete masses are present? Has anyone seen any proof or reference to support using Dunkerley on systems that included distributed masses?
Here are two examples of using Dunkerly on systems that include both discrete and distributed masses that seem to work:
===================EXAMPLE 1 ===============
Let's say we have a a system similar to the Jeffcott rotor: a beam of length L simply supported on both ends with distributed mass (total distributed mass m) and concentrated mas M
From S&V Handbook Chapter 1 page 1.12, we get the answer by adding 50% of the beam mass to the concentrated mass. More specifically:
w^2= 48*E*I / (L^3*<M+0.5*m > )
where the constant 0.6 is not exact... more later.
We also know the solution to the simpler problems of distributed mass alone and lumped mass alone:
w1^2 = Pi^4 * E*I / (m * L^3)
w2^2 = 48 * E*I / (M* L^3)
Applying Dunkerley's equation:
1/w^2 >= 1/w1^2 + 1/w2^2
1/w^2 >= (m * L^3) / (Pi^4 * E*I ) + (M * L^3) / (48 * E*I)
1/w^2 >= ([0.493*m + M]* L^3) / (48 * E*I)
( where we have used 0.493 = 48/Pi^4)
w^2 <= (48 * E*I) / ([0.492767*m+ M]* L^3)
This comes out pretty close to the S&V Handbook Chapter 1 value 0.5 except 0.49... instead of 0.5. But one thing we know about the S&V chapter 1 value is that it is not exact. A method to solve it "exactly" (within the simple Euler beam assumptions) is given in Shock and Vib Handbook chapter 7. That gives the results are tabulated below. The first column is the mass ratio m/M and the second column is that number close to 0.5 (call it X) :
m/M X
0.001 0.4857168063
0.01 0.4857480390
0.1 0.4860378548
0.2 0.4863333819
0.5 0.4870836626
1 0.4880107197
2 0.4891832972
5 0.4907094280
10 0.4915643189
100 0.4926253580
1000 0.4927527114
It looks to me like these stay below the 0.492767=48/Pi^4 for all values, and only approach this limiting value 0.492767 as m/M gets very high (the latter part is expected since the beam approaches the continuous case when m/M gets very high).
So the approach above resulted in a number slightly too high in the denominator which corresponds to a frequency that was slightly too low, which is what we expect for the Dunkerley method.
============= EXAMPLE 2 ========================
Beam supported from fixed/cantilevered support at left side, beam has total distributed mass m uniformly dstributed over length of the beam and concentrated mass M at the end of the beam.
From S&V Handbook Chapter 1 page 1.12, we get the answer by adding 50% of the beam mass to the concentrated mass. More specifically:
w^2= 3*E*I / (L^3*<M+0.23*m > )
I'm not sure how exact the 0.23 number is.
Let's solve using Dunkerley
w1 = resonant frequency of the distributed mass W1 per unit length.
w1^2 = 12.4*E*I/(m*L^3)
w2 = resonant frequency of the concentrated mass W2 at position a.
w2^2 = 3*E*I/(W2*a^3)
1/w^2 = 1/w1^2 + 1/w2^2
1/w^2 = (m*L^3) / (12.4*E*I) + (M*L^3) / (3*E*I)
1/w^2 = (0.24*m +M )*L^3 / ( 3*E*I) (note we have used 0.24 = 3/12.4)
w^2 = ( 3*E*I) / (L^3*<0.24*m +M> )
This is pretty close to what comes from the S&V handbook, just a 0.24 instead of 0.23. Again a higher number in the denominator gives a lower resonant frequency which is what we expect from Dunkerley
===============================
Based on two these two data points (two solved examples above), we might conclude that the Dunkerley approach works to give a frequency slightly below the correct frequency, even when we include distributed mass. Is this always the case? Any proof?
=====================================
Eng-tips forums: The best place on the web for engineering discussions.
1/w^2 = 1/w1^2 + 1/w2^2 + ....
The only proof I have seen of Dunkerley's method uses discrete masses. But it seems that Dunkerely gives a good estimate of the natural frequency for several systems that include distributed mass (examples below). Does Dunkerley apply for systems that include distributed masses? Is the resulting calculated frequencies always a lower bound as it is when only discrete masses are present? Has anyone seen any proof or reference to support using Dunkerley on systems that included distributed masses?
Here are two examples of using Dunkerly on systems that include both discrete and distributed masses that seem to work:
===================EXAMPLE 1 ===============
Let's say we have a a system similar to the Jeffcott rotor: a beam of length L simply supported on both ends with distributed mass (total distributed mass m) and concentrated mas M
From S&V Handbook Chapter 1 page 1.12, we get the answer by adding 50% of the beam mass to the concentrated mass. More specifically:
w^2= 48*E*I / (L^3*<M+0.5*m > )
where the constant 0.6 is not exact... more later.
We also know the solution to the simpler problems of distributed mass alone and lumped mass alone:
w1^2 = Pi^4 * E*I / (m * L^3)
w2^2 = 48 * E*I / (M* L^3)
Applying Dunkerley's equation:
1/w^2 >= 1/w1^2 + 1/w2^2
1/w^2 >= (m * L^3) / (Pi^4 * E*I ) + (M * L^3) / (48 * E*I)
1/w^2 >= ([0.493*m + M]* L^3) / (48 * E*I)
( where we have used 0.493 = 48/Pi^4)
w^2 <= (48 * E*I) / ([0.492767*m+ M]* L^3)
This comes out pretty close to the S&V Handbook Chapter 1 value 0.5 except 0.49... instead of 0.5. But one thing we know about the S&V chapter 1 value is that it is not exact. A method to solve it "exactly" (within the simple Euler beam assumptions) is given in Shock and Vib Handbook chapter 7. That gives the results are tabulated below. The first column is the mass ratio m/M and the second column is that number close to 0.5 (call it X) :
m/M X
0.001 0.4857168063
0.01 0.4857480390
0.1 0.4860378548
0.2 0.4863333819
0.5 0.4870836626
1 0.4880107197
2 0.4891832972
5 0.4907094280
10 0.4915643189
100 0.4926253580
1000 0.4927527114
It looks to me like these stay below the 0.492767=48/Pi^4 for all values, and only approach this limiting value 0.492767 as m/M gets very high (the latter part is expected since the beam approaches the continuous case when m/M gets very high).
So the approach above resulted in a number slightly too high in the denominator which corresponds to a frequency that was slightly too low, which is what we expect for the Dunkerley method.
============= EXAMPLE 2 ========================
Beam supported from fixed/cantilevered support at left side, beam has total distributed mass m uniformly dstributed over length of the beam and concentrated mass M at the end of the beam.
From S&V Handbook Chapter 1 page 1.12, we get the answer by adding 50% of the beam mass to the concentrated mass. More specifically:
w^2= 3*E*I / (L^3*<M+0.23*m > )
I'm not sure how exact the 0.23 number is.
Let's solve using Dunkerley
w1 = resonant frequency of the distributed mass W1 per unit length.
w1^2 = 12.4*E*I/(m*L^3)
w2 = resonant frequency of the concentrated mass W2 at position a.
w2^2 = 3*E*I/(W2*a^3)
1/w^2 = 1/w1^2 + 1/w2^2
1/w^2 = (m*L^3) / (12.4*E*I) + (M*L^3) / (3*E*I)
1/w^2 = (0.24*m +M )*L^3 / ( 3*E*I) (note we have used 0.24 = 3/12.4)
w^2 = ( 3*E*I) / (L^3*<0.24*m +M> )
This is pretty close to what comes from the S&V handbook, just a 0.24 instead of 0.23. Again a higher number in the denominator gives a lower resonant frequency which is what we expect from Dunkerley
===============================
Based on two these two data points (two solved examples above), we might conclude that the Dunkerley approach works to give a frequency slightly below the correct frequency, even when we include distributed mass. Is this always the case? Any proof?
=====================================
Eng-tips forums: The best place on the web for engineering discussions.