TM 1-320  43  AIRSHIP AERODYNAMICS  TABLE  V .-Aerodynamic forces, shear, and bending moments in  U.  S.  S. ZR- 1 at 85 foot/seconds and 5°  42’ pitch  j.  T o determine total shear or bending m<?ment at any frame, it is  necessary to add results obtained from static loading to those computed  from aerodynamic forces.  Turning  Unbal- I  I  Bending  ’  anced  I  moment  Station meters  forces  ’  L  Load  Shear  static  I  ’  .  on hull  I  10  weights  1  pounds  I - 1  Pounds  ,  Pounds  o ________________ _  -820  -57  - 877  0  ~---- ---- .  -------- 10 _____ ____________  - 1,032  - 179  0 2, 3oo  1  l.  089  - 877  -8, 770  20 __ __ ____ ___ ______  -1, 200  - 334  I  2, 300  !  766  212  -6,650  ao _____ ____________ $_{-1, 228 }$ -500  3. 754  2.026  978  3, 130  40 _____ ____ __ __ ____  - 1, 180  - 665  I  4. 937  30 092  3, 004  33, 170  0  ’ 50 _____ ____ ___ __ ___  -985  ..:.... 816  I  2, 300  499  6. 096  I 94, 130  60 _____ ________ ____  - 755  - 933  - 1. 688  I  6, 595  160, 080  -- ------ I  70 _________ ____ ____  - 494  - 1, 020  ---- ---- - 1, 514  4, 907  209,  1~ 0  80 _______ __ ___ ___ __  - 151  - 1,067  -------- -1. 218  3. 393  243,080  90- ---------------- - 55  - 1, 077  ------- - - 1. 132  2, 175  264,830  100 _____ ____ ______ __  0  - 1, 077  -------- -1.077  1, 043  275, 260  110 _____ _____ _______  0  - 1,077  - 1, 077  - 34  274, 920  120 ________________ _  0  - 1, 077  -------- -1.077  - 1. 111  263,810  130 ____________ _____  41  - 1, 077  ----- --- -1. 036  - 2, 188  241, 930  140 _____ ___ ___ ____ __  151  - 1, 067  -------- - 916  - 3, 224  209, 0690  150 _____ __ _____ ___ __  494  -1, 030  -- ------ -536  - 4, 140  168, 290  -L60 _____ _______ ___ __  851  - 933  -------- - 82  - 4, 676  121, 530  170- - - - - - - - - - - - - - - . - 1,346  - 783  --- ----- 563  - 4, 758  73, 950  180 _________ ________  1,891  -563  ------ -- 1, 328  - 4, 195  32, 000  188 ____________ _____  1, 780  - 250  ------ --,  1, 530  - 2, 867  9,020  194.75 __ , - - -0 -------- 1. 346  - 9  .  1. 337  -1. 337  0  -- ---- -- ,  -15,591  15.  591  000  I  I 