Report of committee for year 1929-1930: On Problem of Hydrodynamic Stability -- I. Uniform Shearing Motion in Viscous Fluid, R. V. SOUTHWELL and L. CHITTY; Equations of Motion of Viscous Fluid in Tensor Notation, C. N. H. LOCK; Approximate Solutions of Boundary Layer Equations, V. M. FALKNE R and S. W. SKAN; Flow in Boundary Layer of Airship Model, L. F. G. S IMMONS; Boundary Layers and Drags of Two Streamline Bodies, E. OWER and C. T. HUTTON; Flow Through Pipe Orifices at Low Reynolds Numbers, F. C. JOHANSEN; Effects of Turbulence and Surface Roughness on Drag of Circular Cylinder, A. FAGE and J. H. WARSAP; Viscous Layer Associated with Circular Cylinder, J. J. GREEN; Tests Under Conditions of Infinite Aspect Ratio of 4 Airfoils in High-Speed Wind Channel, T. E. STANTON; Distribution of Pressure Over Symmetrical Joukowski Section at High Speeds, T. E. STANTON; Maximum Lift Coefficient of "Starling" with Clark YH Wings, R. P. ALSTON; Pressure Distribution Over Yawed Airfoil, D. H. WILLIAMS, with Appendix on Rolling Moments on Yawed Airfoil, A. S. BATSON; Experiments on Series of Symmetrical Joukowski Sections, A. FAGE, V. M. FALKNER and W. S. WALKER; Wind Tunnel Tests on Symmetrical Airfoil (Goettingen 429 Section), W. G. A. PERRING; Full Scale Maximum Lift Coefficient of R.A.F. 28 Section Wing, E. T. JONES and K. W. CLARK; Stresses and Strains in Airscrews with Particular Reference to Twist, R. McK. WOOD and W. G. A. PERRING; Distribution of Pressure Over Section of Airscrew Blade in Flight, and Variation of Lift Coefficient with Speed of Section, E. T. JONES; Exploration of Flow Near Screw Proposed for N.P.L. Compressed Air Tunnel, C. N. H. LOCK and A. R. COLLAR; Wind Tunnel Tests with High Speed Airscrews. Experimental Investigation of Blade Twist under Load, G. P. DOUGLAS, W. G. A. PERRING and R. A. FAIRTHORNE; Full Scale Experiments on High Tip Speed Airscrews. Comparative Performance Trials of Three Airscrews of Different Sections, W. G. JENNINGS; Effect of Body Interference on Efficiency of Airscrew, C. N. H. LOCK; Application of Theoretical Velocity Field Round Spheroid to Calculate Performance of Airscrew near Nose of Streamline Body, C. N. H. LOCK; Pressure Plotting Streamline Body with Tractor Airscrew Running -- Part II -- Airscrew in Rear Position, C. N. H. LOCK and F. C. JOHANSEN; Flutter of Airscrew Blades; E. LYNAM; Charts for Aircraft Performance Reduction, H. L. STEVENS and A. E. W. NUTT Method of Calculating Suitable Airscrew Characteristics to Meet Given Conditions; Resulting Airscrew Performance. Part II. Comparison of Observed Change of Performance Consequent on Change of Airscrew and Change Predicted by Methods of Part I, R. S. CAPON; Effect of Span on Aircraft Performance, W. G. JENNINGS; Flight Tests on Variation of Range of Aircraft with Speed and Height, C. E. MAITLAND and A. E. W. NUTT, Moments and Forces on Yawed Model Airplane, W. G. A. PERRING and C. CALLEN; Effect of Altitude Upon Distance Required for Aircraft to Take Off and Climb 20 Meters, Giving Generalized Curves of Weight Reduction Necessary if Given Aircraft is to Comply With Requirements of A. P. 1208 Under Adverse Atmospheric Conditions, K. T. Spencer; Reduction of Drag of Radial Engines by Attachment of Rings of Airfoil Section, H. C. H. TOWNEND; Interference of Wind Tunnel on Symmetrical Body, C. N. H. LOCK; Wind Tunnel Tests of Seven Struts, A. S. HARTSHORN; Comparison of Calculated and Measured Elasticity of Wings of Aircraft, in Connection with Investigation of Wing Flutter, K. T. SPENCER and D. SEED; Stresses in Wing Structures. Accelerometer and Incidence Measurements in Various Manoeuvres, S. S COTT-HALL; Accelerations of Fairey "Flycatcher" Seaplane During Aerobatic Manoeuvres, L. P. COOMBES and A. S. CROUCH; Generalised Curves for Accelerated Motion of Airplane, H. GLAUERT; Measurement of Landing Loads, E. T. JONES; Stresses in Radially Spoked Wire Wheel Under Loads Applied to Rim, A. J. S. PIPPARD and W. E. FRANCIS. (1 pound, 17 shillings, 6 pence)
Technical report of aeronautical research committee 1929-30
Aerodynamics
Aerodynamics ; I
1931
727 pages
Figs., Diagrs., Tables, Plates
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Technical report of Aeronautical Research Committee, 1929-30
Engineering Index Backfile | 1931
Technical report / Aeronautical Research Committee
TIBKAT | 1920/21(1924) - 67.1945(1955)
|Technical report of Aeronautical Research Committee 1938
Engineering Index Backfile | 1947
Technical Report of Aeronautical Research Committee 1930-31
Engineering Index Backfile | 1932
Technical report of Aeronautical Research Council
Engineering Index Backfile | 1955