From the Rolls-Royce experimental archive: a quarter of a million communications from Rolls-Royce, 1906 to 1960's. Documents from the Sir Henry Royce Memorial Foundation (SHRMF).
List of technical reports from the Tenth Annual Report (1924) with authors, titles, and prices.
| Identifier | ExFiles\Box 76\3\ scan0244 | |
| Date | 1st January 1924 | |
| - 18 - NO. PRICE TENTH ANNUAL REPORT (1924) (Administrative Report, without technical reports) $ .15 TENTH ANNUAL REPORT (1924) (Containing Reports Nos. 186 to 209) 186 APPLICATION OF PROPELLER TEST DATA TO DESIGN AND PERFORMANCE CALCULATIONS. By Walter S. Diehl........... .05 187 FLAME SPEED AND SPARK INTENSITY. By D.{John DeLooze - Company Secretary} W. Randolph and F.{Mr Friese} B. Silsbee. ............................ .10 188 THE INFLUENCE OF THE FORM OF A WOODEN BEAM ON ITS STIFFNESS AND STRENGTH - III: STRESSES IN WOOD MEMBERS SUBJECTED TO COMBINED COLUMN AND BEAM ACTION. By J.{Mr Johnson W.M.} A.{Mr Adams} Newlin and G.{Mr Griffiths - Chief Accountant / Mr Gnapp} W. Trayer........ .05 189 RELATION OF FUEL-AIR RATIO TO ENGINE PERFORMANCE. By Stanwood W. Sparrow. ........................ .10 190 CORRECTING HORSEPOWER MEASUREMENTS TO A STANDARD TEMPERATURE. By Stanwood W. Sparrow............. .05 * 191 ELEMENTS OF THE WING SECTION THEORY AND OF THE WING THEORY. By Max M.{Mr Moon / Mr Moore} Munk. ........................ .10 192 CHARTS FOR GRAPHICAL ESTIMATION OF AIRPLANE PERFORMANCE. By Walter S. Diehl. .................... .05 193 PRESSURE DISTRIBUTION OVER THE WINGS OF AN MB-3 AIRPLANE IN FLIGHT. By F.{Mr Friese} H.{Arthur M. Hanbury - Head Complaints} Norton............... .15 194 INVESTIGATION OF SLIPSTREAM VELOCITY. By J.{Mr Johnson W.M.} W. Crowley, Jr.{Mr James Royce} ................................... .05 195 STANDARDIZATION TESTS OF N.A.C.A. NO. 1 WIND TUNNEL. By Elliott G.{Mr Griffiths - Chief Accountant / Mr Gnapp} Reid. ............................ .10 196 COMPARISON OF MODEL PROPELLER TESTS WITH THE AIRFOIL THEORY. By W. F.{Mr Friese} Durand and E.{Mr Elliott - Chief Engineer} P. Lesley.... .10 197 A NEW RELATION BETWEEN THE INDUCED YAWING MOMENTS AND THE ROLLING MOMENTS OF AN AIRFOIL IN STRAIGHT MOTION. By Max M.{Mr Moon / Mr Moore} Munk. ........................ .05 198 ASTRONOMICAL METHODS IN AERIAL NAVIGATION. By K.{Mr Kilner} Hilding Beij. ................................ .15 * Available only in annual report. | ||