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    Title :

    Aeronautics. Tenth annual report of the National Advisory Committee for Aeronautics, 1924. Including technical reports Nos. 186 to 209




    Publication date :

    1925


    Size :

    Online-Ressource (508 p)


    Remarks:

    illustrations, tables
    Campusweiter Zugriff (Universität Hannover) - Vervielfältigungen (z.B. Kopien, Downloads) sind nur von einzelnen Kapiteln oder Seiten und nur zum eigenen wissenschaftlichen Gebrauch erlaubt. Keine Weitergabe an Dritte. Kein systematisches Downloaden durch Robots.
    Appendix to Technical Report No. 190, p. 137
    Index to Technical Report No. 206, p. 421
    List of illustrations in Technical Report No. 198, p. 272
    Table of contents for Technical Report No. 198, p. 271
    Table of contents, p. VII
    Technical Report No. 186. The application of propeller test data to design and performance calculations, by Walter S. Diehl, p. 67
    Technical Report No. 187. Flame speed and spark intensity, by D.W. Randolph and F.B. Silsbee, p. 79
    Technical Report No. 188. Stresses in wood members subjected to combined column and beam action, by J.A. Newlin and G.W. Trayer, p. 93
    Technical Report No. 189. Relation of fuel-air ratio to engine performance, by Stanwood W. Sparrow, p. 107
    Technical Report No. 190. Correcting horsepower measurements to a standard temperature, by Stanwood W. Sparrow, p. 123
    Technical Report No. 191. Elements of the wing section theory and of the wing theory, by Max M. Munk, p. 139
    Technical Report No. 192. Charts for graphical estimation of airplace performance, by Walter S. Diehl, p. 165
    Technical Report No. 193. Pressure distribution over the wings of an MB-3 airplane in flight, by F.H. Norton, p. 177
    Technical Report No. 194. Investigation of slipstream velocity, by J.W. Crowley, Jr., p. 197
    Technical Report No. 195. Standardization tests of N.A.C.A. No. 1 wind tunnel, by Elliott G. Reid, p. 205
    Technical Report No. 196. Comparison of model propeller tests with airfoil theory, by William F. Durand and E.P. Lesley, p. 235
    Technical Report No. 197. A new relation between the induced yawing moment and the rolling moment of an airfoil in straight motion, by Max M. Munk, p. 261
    Technical Report No. 198. Astronomical methods in aerial navigation, by K. Hilding Beij, p. 269
    Technical Report No. 199. Interference tests on an N.A.C.A. pitot tube, by Elliott G. Reid, p. 321
    Technical Report No. 200. Some problems on the lift and rolling moment of airplane wings, by James B. Scarborough, p. 329
    Technical Report No. 201. The effects of shielding the tips of airfoils, by Elliott G. Reid, p. 345
    Technical Report No. 202. The sparking voltage of spark plugs, by F.B. Silsbee, p. 355
    Technical Report No. 203. Accelerations in flight, by J.H. Doolittle, p. 371
    Technical Report No. 204. Forces on airships in gusts, by C.P. Burgess, p. 389
    Technical Report No. 205. The effect of changes in compression ratio upon engine performance, by Stanwood W. Sparrow, p. 397
    Technical Report No. 206. Nonmetallic diaphragms for instruments, by H.N. Eaton and C.T. Buckingham, p. 419
    Technical Report No. 207. Aerodynamic characteristics of airfoils at high speeds, by L.J. Briggs, G.F. Hull, and H.L. Dryden, p. 463
    Technical Report No. 208. A determination of turning characteristics of the C-7 airship by means of a camera obscura, by J.W. Crowley, Jr., and R.G. Freeman, p. 481
    Technical Report No. 209. Characteristics of a single float seaplane during take-off, by J.W. Crowley, Jr. and K.M. Ronan, p. 489
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    Type of media :

    Book


    Type of material :

    Electronic Resource


    Language :

    English