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Memorandum DCL-ISl Page -1" ':of 12(\?

SUBJECT:

To:

From:

Digital Computer Laboratory Massachusetta "Institute of Technology

Cambridge 39, Massachusetts

___

----~~---::::-::-:;-;::-"""l BIWEEKLY ItEPORT, OC'l'OBER28.

U~6 LIN. LAB. DtV. 6

Frank II. Verzull.

DOCU M ENT ROOM.:

SCientific and Eng1neerug Comp . t i t S

GM

U

0 T REM 0 V t I

1. MATHEMATICS, CODING AND APPLICATIONS

FHOM

1.1 Introduction

1H'S R'OOM

During the pa~t two weeks A~I=:. ,...J ... "" .. "_ were run on the time allocated to the Seli:'entific and Engineering (S and Ee) Group. These programs represent part of the work that has been done

"on 48 of the problems that have been accepted by theS"and,EC Group.

1.2 Programs and Computer Operation Problem.No.

100 126 D.

131 141 162 li'.

193 L.

199 N.

203 DgN.

204 N.

219

225 B,N.

226 D.

231 B,N.

253 N.

"257 C.

260 N.

261 C.

262 NT 264 C.

'273 N.

274 N.

278 N.

3,06 D.

309 B,N.

310 C.

Title

Comprehensive System of Service Routines Data Reduction

Special Problems (Staff Trainin" etc.) S and EC Subroutine Study

Nuclear'~ Sea ttering ~hase-Sh1fts

,E. V. Problem for Propagation of E. ~. Waves Compressible Flow in a Tube

Response of a Building Under Dynauaic Loading Exchange Integrals Between Real Slat~r 9rbitals'.

Linear Programming

~Neutron-Deurteron Scattering Circulation 'of the Atmosphere Reactor RJnaway Prevention

AJ?W

as Applied to 'Face- anq. Body-Centered Iron Horizontal Stabilizer Analysis ,

Energy,Levels of Diatomic Hydrides.

Fourier'Synthes'is :for Crystal Stru~tures Evalu~tion of' Two-oenter Molecular .,lx;ltegrals ' Opt'ilnization of Alternator Control System Cosmic

Ray

Air Show$r

Multiple Scattering

Energy Levels of Diatomic Hydrides LiB Spectral Analysis "of' Atmospher1-C Data Pure 'and '~pure Potassium C~IQride Cr,ystal Rocket \ Trajecto,ry CalQU.lat:LOns '

Minutes'

-150.7 190.3 '393.5 25.3 12.1 178.8 72.8 29.1

,2~6 03 49.6 47.2 45.9' 11.2' '20.9 177.9 13.5 27.6 47.1 4.2 , 36~.6

. 30.8 159.6 , 11.2 l4!S '35.3

(2)

DeL-15I

312 L.

317 C.

327 L.

336 C.

337 N.

341 C'.

343 C •.

354 D.

361 B.N.

364 C.

368 B,N.

369 372 B.

377 L.

382 B.

383 C.

385 B.

386 C.

387 C.

388 D.

391 L.

393 N.

394 C.

Error Analysis

Stability Derivatives from Flight Test Data 'Prediction Analysis

Pattern Identification

Nonlinear 2nd Order Diff. Eqs.

Statistical and Dynamic Methods in.Forecasting Weather Prediction

Response of a Single Story Concrete Building Growth of Fatigue Cracks

Blast Re~ponse of Rotor Blades Condensation in

a

Vertical Tube Temperature Distribution in a Beam Design of Spherical Shell Segments Coverage Analysis

Calculation of Prime Numbers Stokes Particle Velocities Feed Plate Location

Free Convection

Determination of Velocity Potential

Tem.perature Distribution in Aircraft Generators Magnetic Relaxation in Thin Films'

The Inverse Bremsstrahlung Spectrum

Autonmat1c Programming for Numerically Controlled Machine Tools

1.3 Computer Time Statistics

Page 2 21.2

93.7 175.9 40.7

10.5

264.7 3.8 8.7 19.9 42.1 4.1 308.7 23.9 54.0 32.7

22 . .3 ~

22.1 2.3 1.7 37.7 23.9 2.7 8.7

The following indicates the distribution of WWI time allo- cated to the Sand EC Group.

S and ~C Programs Lincolp Program$

Magnetic Tape Te~t

Scope Calibration . PETR Test

Test Storage Check

, DeJ!lloIllstrations (No. 131)

Total Time Logged Division 6 Conversion"

Inter-run OperatioDS, etc.

Total Time Assigned

U~able ~imep Percentage

N~ber of Programs

46 Bra.

7 Brs.

6 Brs.

62 Bra.

5 Bra.

;69 Hr ••

96.47' 455

51.9 min.

9.9 min.

54.1 min.

12.2 min.

27.7 min .

7.2 min.

33.5 m.in.

1605 mine

13.8 min.

58.3 min.

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