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Squire, L.C.

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Reports and memoranda. №3373 : Pressure distributions and flow patterns at M=4.0 on some delta wings
1964
Squire L.C.
2324
0
Reports and memoranda. №3310 : Further experimental investigations of the characteristics of cambered gothic wings at Mach numbers from 0.4 to 2.0
1963
Squire L.C.
2659
0
Current papers. №673 : Measurements of lift and pitching moment of four ogee wings at supersonic speeds
1964
Squire L.C.
994
0
Current papers. №924 : Camber effects on the non-linear lift of slender wings sharp leading edges
1967
Squire L.C.
948
0
Reports and memoranda. №3278 : Some applications of hot-so-slender wing theory to wings with curved leading
1962
Squire L.C.
2831
0
Reports and memoranda. №3340 : Pressure distribution and flow patterns on some conical shapes with sharp edges and symmetrical cross-sections at M=4.0
1963
Squire L.C.
2835
0
Reports and memoranda. №3305 : An experimental investigation of the characteristics of some plane and cambered 65º delta wings at Mach numbers from 0.7 to 2.0
1963
Squire L.C.
2378
0
Current papers. №585 : En experimental investigation of the characteristics of an ogee wing from M=0.4 to M=1.8
1962
Squire L.C.
1636
0
Current papers. №395 : The influence of a model on plenum chamber indication of Mach number in a slotted wall wind tunnel
1958
Squire L.C.
932
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Current papers. №740 : Some notes en turbulent boundary layers with fluid injection at high supersonic speeds
1964
Squire L.C.
2686
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The boundary layer development downstream of a shock interaction at an expansion corner
1979
Chew Y. T., Squire L.C.
814
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Current papers. №864 : Approximate formulae for the lift and drag of wedge aerofoil sections at high supersonic speeds
1966
Squire L.C.
2989
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Reports and memoranda. №3370 : The characteristics of some slender cambered gothic wings at Mach numbers from 0.4 to 2.0
1964
Squire L.C.
1517
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