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  • Virtual Principles in Aircraft Structures (Mechanics of Structural Systems) (v. 1)
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Buy from Amazon $134.25$63.99 $150.00 $116.67 $83.33 $50.00 Nov Dec Jan Feb Mar Apr May 2016 $99.00, Oct 14 - Apr 15$89.10, Oct 14 - Nov 15$99.00, Oct 14 - Apr 15$89.05, Nov 19 8:27 pm$99.00, Oct 14 - Apr 15$88.91, Nov 24 6:57 am$99.00, Oct 14 - Apr 15$88.79, Nov 28 10:34 pm$99.00, Oct 14 - Apr 15$89.10, Dec 3 - Dec 8$99.00, Oct 14 - Apr 15$89.01, Dec 13 8:27 pm$99.00, Oct 14 - Apr 15$89.10, Dec 18 - Dec 23$99.00, Oct 14 - Apr 15$69.99, Dec 28 - Jan 2$99.00, Oct 14 - Apr 15$70.00, Jan 7 12:15 pm$99.00, Oct 14 - Apr 15$69.99, Jan 12 10:48 am$99.00, Oct 14 - Apr 15$69.98, Jan 17 - Jan 22$99.00, Oct 14 - Apr 15$69.97, Jan 27 - Feb 1$99.00, Oct 14 - Apr 15$64.00, Feb 6 2:11 pm$99.00, Oct 14 - Apr 15$63.99, Feb 11 - Feb 27$99.00, Oct 14 - Apr 15$94.02, Mar 11 12:51 pm$134.25, Mar 23 9:42 am$99.00, Oct 14 - Apr 15$134.05, Apr 3 9:36 pm$99.00, Oct 14 - Apr 15$133.93, Apr 15 1:57 pm$99.00, Oct 14 - Apr 15 6,872,5417,786,121 7,421,875 7,031,250 6,640,625 Nov Dec Jan Feb Mar Apr May 2016

Price Details

New

Latest $99.00 Apr 15, '16
Highest $99.00 Oct 14, '15
Lowest $99.00 Oct 14, '15
Average $99.00 (30d avg)
$99.00 (90d avg)
$99.00 (180d avg)
$99.00 (Lifetime average)
Added Oct 14, 2015

3rd Party Used

Latest $133.93 Apr 15, '16
Highest $134.25 Mar 23, '16
Lowest $63.99 Feb 11, '16
Average $134.15 (30d avg)
$87.57 (90d avg)
$86.25 (180d avg)
$86.31 (Lifetime average)
Added Oct 14, 2015

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30 day average: 7,752,267
90 day average: 7,583,605

Product Description

The basic partial differential equations for the stresses and displacements in clas sical three dimensional elasticity theory can be set up in three ways: (1) to solve for the displacements first and then the stresses; (2) to solve for the stresses first and then the displacements; and (3) to solve for both stresses and displacements simultaneously. These three methods are identified in the literature as (1) the displacement method, (2) the stress or force method, and (3) the combined or mixed method. Closed form solutions of the partial differential equations with their complicated boundary conditions for any of these three methods have been obtained only in special cases. In order to obtain solutions, various special methods have been developed to determine the stresses and displacements in structures. The equations have been reduced to two and one dimensional forms for plates, beams, and trusses. By neglecting the local effects at the edges and ends, satisfactory solutions can be obtained for many case~. The procedures for reducing the three dimensional equations to two and one dimensional equations are described in Chapter 1, Volume 1, where the various approximations are pointed out.

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