Flight Experiments on Boundary Layer Transition in Relation to Profile Drag, A. V. STEPHENS and J. A. G. HASLAM, p 45-99; Experiments on Transition of Laminar Boundary Layer on Flat Plate, A. A. HALL and G. S. HISLOP, p 100-26; Critical Reynolds Numbers of Spheres in Compressed Air Tunnel, A. FAGE and D. H. WILLIAMS, p 127-33; Measurements of Intensity and Scale of Turbulence, A. A. HALL, p 135-72; Longitudinal Flow in Trailing Vortex, W. F. HILTON, p 173-6; Flight Tests on Wing Sections Using Parasol Monoplane, p 177-95; Calculation of Profile Drag of Aerofoils, H. B. SQUIRE and A. D. YOUNG, p 196-222; Experiments on Riveted Wing in Compressed Air Tunnel, D. H. WILLIAMS and A. F. BROWN, p 247-50; Flight Tests of Falcon Fitted with Irving Flap, J.COHEN and H. P. FRASER, p 251-65; Tests on 16 Per Cent HandleyPage Aerofoil with 20 Per Cent Slotted Flap in Compressed Air Tunnel, D. H. WILLIAMS, A. H. BELL and E. SMYTH, p 266-83; Investigation Into Characteristics of C.30A Autogiro, P. HUFTON, A. E. WOODWARD NUTT, F.J. BIGG and J. A. BEAVAN, p 284-346; Graphical Method of Calculating Performance of Airscrew, C. N. H. LOCK, p 354-424; Airscrew Blade Vibration, J. MORRIS, p 425-53; Vibration of Airscrew Blades -- Extension of Theory Given in R and M 1758, B. C. CARTER, p 455-62. (£1 10s net)
Technical report of Aeronautical Research Committee 1938
Technical Report Aeronautical Research Committee
1947
462 pages
Illus, Diagrs, Charts, Tables
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Technical report / Aeronautical Research Committee
TIBKAT | 1920/21(1924) - 67.1945(1955)
|Technical report of Aeronautical Research Committee, 1929-30
Engineering Index Backfile | 1931
Technical report of aeronautical research committee 1929-30
Engineering Index Backfile | 1931
Technical Report of Aeronautical Research Committee 1930-31
Engineering Index Backfile | 1932
British aeronautical research for 1938
Engineering Index Backfile | 1939