| 1 |
Fluid motion (theory)
東京 : 富士出版 , 1944
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| 2 |
no. 769
The calculation of stresses in a redundant structure by the method of comparison of deflections, with examples of its application to aeroplane design / by W. S. Farren ; with a historical preface by H. Lamb
London : Majesty's stationery Office , 1922
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| 3 |
No. 980 (Ae.193)
The rolling and yawing moments of an aerofoil in straight flight / by H. Grauert
London : His Majesty's Stationery Office , 1925
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| 4 |
No. 987 (Ae.199)
The full scale determination of the lateral resistance derivatives of a bristol fighter aeroplane / by H.M. Garner
London : His Majesty's Stationery Office , 1926
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| 5 |
No. 990 (Ae.201)
Full scale and model measurements of lift and drag of bristol fighter with R.A.F. 31 wings / by B.D. Clark
London : His Majesty's Stationery Office , 1926
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| 6 |
No. 1155
The flutter of aeroplane wings / by R. A. Frazer and W. J. Duncan
Londn : H. M.'s Stationery Off. , 1929
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| 7 |
no. 1255. Jan., 1931
The flutter of monoplanes biplanes and tail units : (A sequel to R.& M.1155) / R. A. Frazer and W. J. Duncan
London : His Majesty's Stationery Off. , 1931
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| 8 |
no. 1433
Corrosion fatigue test on aluminium crystal / by H.J. Gough, D.G. Sopwith
London : His Majesty's Stationery Office , 1932
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| 9 |
no. 2884
Methods for calculating the lift distribution of wings : subsonic lifting-surface theory / by H. Multhopp
東京 : PBリポート社 , [19--]
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| 10 |
no. 2935
A simple method for calculating the span and chordwise loading on straight and swept wings of any given aspect ratio at subsonic speeds / by D. Küchemann
東京 : PBリポート社 , [19--]
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