Research in Resistance and Propulsion
... draftwise distribution m ( , ) = m1 ( 5 ) . m2 ( ζ ) where = = m2 ( 5 ) = 1 - ᅵ ᅵ +1 u = - 1 + 1 4πτ - +1 V = 1 4πt -1 X 5 ) ( rt + r_t m1 ( 5 ) ( x = -25 ) ( rt m1 ( 5 ) ... Draftwise Distribution ii) Parabolic Draftwise Distribution.
B Series Publications
... draftwise , f2 ( ζ ) = 1 ( -t ≤5 ≤ t ) -t -1 1 f = 4π + the velocity components become - 4πυ = 4π - tl f1 ( g ) ( x - 5 ) αξ αζ 2 [ ( x - 5 ) 2 + y2 + ( z - 5 ) 2 ] 3/2 ( 5 ) ( x - 5 ) ( z - t z + t ) de ( x - 5 ) 2 + y2 r - r ' -1 t1 ...
Future-Proof Legal Services
... Draftwise www.draftwise.com/ Legal Search; 1. Allows legal teams to find terms, definitions and documents with specific language. Filters such as DMS, client, document type, author, or last modified date improve search accuracy ...
Proceedings
... draftwise uniform strength . The above mentioned type of distribution for representing a ship has been the object of various complaints not only from naval architects but also from theorists . The most serious point is that the hull ...
International Seminar on Theoretical Wave-Resistance
... draftwise uniform strength . The above mentioned type of distribution for representing a ship has been the object of various complaints not only from naval architects but also from theorists . The most serious point is that the hull ...
Publication
... draftwise direction ( i.e. = 0 and as N = 1 ) , and we divide the ship into 20 equal intervals ( i.e. M = 20 ) in the fore - and - aft direction . In other words , the center plane source distribution is divided onto the MxN = 20 ...
Schiffstechnik
... draftwise expression in Fig.15 . Since the difficulty of pressure measurements increases with lowering the Fn and the model size , Fn = 0.13 may be regarded as a lower limit for a 2.5m model ( Cp = 0.1 amounts to about 2mmAq . in this ...
CORRELATION OF LONGITUDINAL WAVE PROFILES AND THE WAVE RESISTANCE OF A SHIP MODEL, WITH A PROPOSED LOCAL-DISTURBANCE CORRECTION.
... draftwise direction ( i.e. N = 1 ) , and we divide the ship into 20 equal intervals ( i.e. M = 20 ) in the fore - and - aft direction . In other words , the center plane source ১৭ ( ६ , ९ ) = 0 and ১ ९ distribution is divided onto ...
First Symposium on Ship Maneuverability
... draftwise : * T2 T1 1 = 1.11 0.9 The model scales were respectively 1 / 66.67 and 1 / 74.07 . ** The following tests have been carried out : On the two forms , measurements of forces on the bare hull and on the hull provided with a ...
Report - Naval Ship Research and Development Center
... draftwise : = 1.20 ; and - T1 B3 Form 3 is obtained by expansion * of Form 1 beamwise : = 1.20 . B1 The models had a length of 2.50 m ; they were fitted with turbulence pins . The following tests have been done : measurements of forces ...
Chironian
... DRAFT . WISE regulation has been approved by President Wil- son governing the operation of the Selective Draft Law upon hospital internes and medical students who have been more than a year in college . The inadvisability of using such ...
Mathematics, Physics, Chemistry, and Engineering
... Draftwise distribution of wave - free singularity ( 5.6 ) with an arbitrary function m ( x ) , then u ( x , z ) may be calculated as shown in Fig . 4. From these figures , we may easily imagine that the section forms of the ship may be ...
Naval Architecture and Ocean Engineering
... draftwise direction , which represents the lifting action originating from obliquing ( vide . Fig.2 ) . From bound vortex distribution , there should exist trailing vortex which , we assume , sheds from each strip with angle to infinite ...
The Sixth Man
... draftwise , whether they were or were not , because a person who would acknowledge homosexuality , when he wasn't , certainly wasn't acceptable . " For every known homosexual there are again at least fifty not known to any agency ...
Calculations of Ship Hull Forms With Electronic Digital Computers
... draftwise , f2 ( ζ ) = 1 ( -t ≤ ≤ t ) the velocity components become t1 - 4πι = 4π -t - 1 1 4π + -1 - - 4πν = t1 -SS -t -1 1 = + -1 - - f1 ( § ) ( x - ξ ) αξ αζ 2 [ ( x - 5 ) 2 + y2 + ( z - g ) 2 ] 3/2 - f1 ( 5 ) ( x - 5 ) ( z - t z + t ) ...
Memoirs of the Graduate School of Engineering, Kyushu University
... draftwise direction . Expressing the mean bottom of the hull as y1 = -d ( x ) = d + f , where dis mean draft of the hull , and denoting the half apparent momentum thickness of the wake in the plane y1 = constant by the function d2 ( yi ) ...
Memoirs of the Faculty of Engineering, Kyushu University
... draftwise direction . Expressing the mean bottom of the hull as y1 = -d ( x1 ) = d + f , where d is mean draft of the hull , and denoting the half apparent momentum thickness of the wake in the plane y1 = constant by the function d2 ( y ) ...
Memoirs of the Faculty of Engineering, Hiroshima University
... draftwise depth of the distribution plane and c is a constant . Because the difference between the solutions of the first and the second step is small , Eq . ( 35 ) can be written by the aid of the Michell's approximation , -m1 ( x ) ...
Impeachment Inquiry
... draftwise and languagewise , which I think has improved it from , say , old Greek to old English . It is still a little convoluted , and I am really a strong advocate of simple requests for power and I do not feel that we should be ...
Impeachment Inquiry Books I-III: January 31-July 23, 1974
... draftwise and languagewise , which I think has improved it from , say , old Greek to old English . It is still a little convoluted , and I am really a strong advocate of simple requests for power and I do not feel that we should be ...