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).
Index page from the Eighth Annual Report of 1922, listing reports with their numbers, titles, authors, and prices.
| Identifier | ExFiles\Box 76\3\ scan0240 | |
| Date | 1st January 1921 guessed | |
| - 14 - NO. PRICE EIGHTH ANNUAL REPORT (1922) . . . . . . . . . . . . . . . $.10 (Administrative report only - without technical reports) EIGHTH ANNUAL REPORT (1922) . . . . . . . . . . 1.50 (Containing Reports Nos.133 to 158). 133 THE TAIL PLANE. By Max M.{Mr Moon / Mr Moore} Munk. . . . . . . . . . . . . . . . . .10 134 PERFORMANCE OF MAYBACH 300-HORSEPOWER AIRPLANE ENGINE. By S. W. Sparrow. . . . . . . . . . . . . . . . . . . . . . .05 135 PERFORMANCE OF B.M.W. 185-HORSEPOWER AIRPLANE ENGINE. By S. W. Sparrow. . . . . . . . . . . . . . . . . . . . . . .05 136 DAMPING COEFFICIENTS DUE TO TAIL SURFACES IN AIRCRAFT. By Lynn Chu. . . . . . . . . . . . . . . . . . . . . . . . .05 137 POINT DRAG AND TOTAL DRAG OF NAVY STRUTS NO.1 MODIFIED. By A.{Mr Adams} F.{Mr Friese} Zahm, R.{Sir Henry Royce} H.{Arthur M. Hanbury - Head Complaints} Smith and G.{Mr Griffiths - Chief Accountant / Mr Gnapp} C. Hill. . . . . . . . . . . .05 138 THE DRAG OF "C" CLASS AIRSHIP HULL WITH VARYING LENGTHS OF CYLINDRIC MIDSHIPS. By A.{Mr Adams} F.{Mr Friese} Zahm, R.{Sir Henry Royce} H.{Arthur M. Hanbury - Head Complaints} Smith and G.{Mr Griffiths - Chief Accountant / Mr Gnapp} C. Hill. . . . . . . . . . . . . . . . . . . . . . . . .05 139 INFLUENCE OF MODEL SURFACE AND AIR FLOW TEXTURE ON RE- SISTANCE OF AERODYNAMIC BODIES. By A.{Mr Adams} F.{Mr Friese} Zahm. . . . . . . . .05 140 LIFT AND DRAG EFFECTS ON WING TIP-RAKE. By A.{Mr Adams} F.{Mr Friese} Zahm, R.{Sir Henry Royce} M.{Mr Moon / Mr Moore} Bear and G.{Mr Griffiths - Chief Accountant / Mr Gnapp} C. Hill. . . . . . . . . . . . . . . . . . . .05 141 EXPERIMENTAL RESEARCH ON AIR PROPELLERS - V.{VIENNA} By Wm. F.{Mr Friese} Durand and E.{Mr Elliott - Chief Engineer} P. Lesley. . . . . . . . . . . . . . . . . . . .15 142 GENERAL THEORY OF THIN WING SECTIONS. By Max M.{Mr Moon / Mr Moore} Munk. . . . . . .05 143 ANALYSIS OF STRESSES IN GERMAN AIRPLANES. By Wilhelm Hoff. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .15 144 THE DECAY OF A SIMPLE EDDY. By H.{Arthur M. Hanbury - Head Complaints} Bateman. . . . . . . . . . . . .05 145 INTERNAL STRESSES IN LAMINATED CONSTRUCTION. By A.{Mr Adams} L. Heim, A.{Mr Adams} C. Knauss and Louis Seutter. . . . . . . . . . . . . .10 146 THE SIX-COMPONENT WIND BALANCE. By A.{Mr Adams} F.{Mr Friese} Zahm. . . . . . . . . .05 | ||