Reports and Memoranda, Issues 2826-2849H.M. Stationery Office, 1949 - Aeronautics Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list. |
Contents
inertia The critical flutter speed rises with increasing moment of inertia until a transition point | 3 |
REFERENCES | 20 |
No Author Title | 1 |
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Aero and Hydrodynamics aerodynamic aerofoil AERONAUTICAL RESEARCH COUNCIL afterbody aileron Airscrews Appendix applied blade body boundary layer C₁ calculated cavitation cent chord column compressible curves cylinder delta wing direct stress drag effect elevator elevon Engines equation experimental flight flow flutter speed frequency fuselage given incidence increase inertia interference drag leading edge lift coefficient load lower surface Mach number maximum method MINISTRY OF SUPPLY normal mode obtained oscillating parameter parent aircraft pitching pitching moment position pressure distributions ratio rear recovery REPORTS AND MEMORANDA Reynolds number rolling root root chord Seaplanes shear shock-wave shown in Fig span spar Stability and Control stall stiffness Structures supersonic sweepback symmetrical t₁ Table tailplane telemetering temperature test vehicle theory torsion trailing edge upper surface Upper x/c values variation velocity distribution Wind Tunnels wing zero