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).
Price list of aeronautical reports from the Ninth Annual Report (1923).
| Identifier | ExFiles\Box 76\3\ scan0242 | |
| Date | 1st January 1921 guessed | |
| - 16 - NO. PRICE NINTH ANNUAL REPORT (1923) (Administrative Report, without technical Reports).....$.10 NINTH ANNUAL REPORT (1923) (Containing Reports Nos. 159 to 185)..... 1.00 159 JET PROPULSION FOR AIRPLANES. By Edgar Buckingham..... .05 160 AN AIRSHIP SLIDE RULE. By E.{Mr Elliott - Chief Engineer} R.{Sir Henry Royce} Weaver and S. F.{Mr Friese} Pickering. ..... .05 161 THE DISTRIBUTION OF LIFT OVER WING TIPS AND AILERONS. By David L. Bacon. ..... .10 162 COMPLETE STUDY OF THE LONGITUDINAL OSCILLATION OF A VE-7 AIRPLANE. By F.{Mr Friese} H.{Arthur M. Hanbury - Head Complaints} Norton and W. G.{Mr Griffiths - Chief Accountant / Mr Gnapp} Brown.... .05 163 THE VERTICAL, LONGITUDINAL AND LATERAL ACCELERATIONS EXPERIENCED BY AN SE-5A AIRPLANE WHILE MANEUVERING. By F.{Mr Friese} H.{Arthur M. Hanbury - Head Complaints} Norton and T. Carroll. ..... .05 164 THE INERTIA COEFFICIENTS OF AN AIRSHIP IN A FRICTION-LESS FLUID. By H.{Arthur M. Hanbury - Head Complaints} Bateman. ..... .05 165 DIAPHRAGMS FOR AERONAUTIC INSTRUMENTS. By M.D. Hersey. .10 166 THE AERODYNAMIC PLANE TABLE. By a.{Mr Adams} F.{Mr Friese} Zahm......... .05 167 THE MEASUREMENT OF THE DAMPING IN ROLL ON A JN4H IN FLIGHT. By F.{Mr Friese} H.{Arthur M. Hanbury - Head Complaints} Norton. ..... .05 168 THE GENERAL EFFICIENCY CURVE FOR AIR PROPELLERS. By Walter S. Diehl. ..... .05 169 THE EFFECT OF AIRFOIL THICKNESS AND PLAN FORM ON LATERAL CONTROL. By H.{Arthur M. Hanbury - Head Complaints} I. Hoot. ..... .05 170 A STUDY OF LONGITUDINAL DYNAMIC STABILITY IN FLIGHT. By F.{Mr Friese} H.{Arthur M. Hanbury - Head Complaints} Norton. ..... .05 171 ENGINE PERFORMANCE AND THE DETERMINATION OF ABSOLUTE CEILING. By Walter S. Diehl. ..... .05 172 DYNAMIC STABILITY AS AFFECTED BY THE LONGITUDINAL MOMENT OF INERTIA. By Edwin B. Wilson. ..... .05 | ||