Simplified loading formulae for pull-out manoeuvres of tailed aeroplanes /

Bibliographic Details
Main Author:	Neumark, S.
Format:	Book
Language:	English
Published:	London : Her Majesty's Stationery Office, 1963.
Series:	Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3327.
Subjects:	Aerodynamic load.

Similar Items

Aerodynamic loads on external stores : A review of experimental data and method of prediction /
by: Marsden, Philip
Published: (1967)

An iterative method for calculation of the loading on a thin unswept wing /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1973)

The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow /
by: Smith, Jeremy H. B.
Published: (1967)

Low-speed theoretical and experimental aerodynamic loading on highly-swept curved-tipped wings of two thicknesses /
by: Garner, Henry Clifford
Published: (1974)

The load near the apex of a lifting swept wing in linearised subsonic flow /
by: Davies, Patricia J.
Published: (1973)

Calculation of unsteady generalised air-forces on a thin wing oscillating harmonically in subsonic flow /
by: Davies, David Eric
Published: (1965)

On the prediction of base pressure on two-dimensional supersonic turbulent flow /
by: Roberts, J. B. (Writer on aerodynamics)
Published: (1966)

An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street /
by: Nash, John F.
Published: (1966)

The unsteady forces on finite wings in transient motion /
by: Dore, Barrie Dennis
Published: (1967)

Some exact calculations of the lift and drag produced by a wedge in supersonic flow : either directly or by interference /
by: Roe, P. L.
Published: (1967)

Some mutual interference effects between a 5.7 cone and sonic-leading-edge delta wing at M..-2.49 /
by: Goldsmith, E. L.
Published: (1967)

Calculation of the response of a flexible aircraft to harmonic and discrete gusts by a transform method /
by: Mitchell, C. G. B.
Published: (1968)

The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory /
by: Harris, G. Z.
Published: (1967)

A study of dynamic aeroelastic effects on the stability control and gust response of a slender delta aircraft /
by: Broadbent, E. G.
Published: (1972)

Charts of peak amplitudes in incidence and sideslip in rolling manoeuvres due to inertia cross coupling /
by: Pinsker, W. J. G.
Published: (1962)

A contribution to the theory of aircraft response in rolling manoeuvres : including inertia cross-coupling effects /
by: Thomas, H. H. B. M.
Published: (1964)

Equilibrium configurations of flying cables of captive balloons : and cable derivatives for stability calculations /
by: Neumark, S.
Published: (1963)

Lift due to interference between an aerofoil and an external non-lifting body /
by: Neumark, S.
Published: (1965)

The effect of steady tailplane lift on the subcritical response of a subsonic t-tail flutter model /
by: McCue, D. J.
Published: (1971)

Manual on aircraft loads /
by: Taylor, James, 1916-
Published: (1965)

Static instability of rectangular orthotropic panels subjected to uniform in-plane loads and deflection-dependent lateral loads /
by: Johns, David John
Published: (1969)

Simplified three-dimensional analysis and design of fibre reinforced annular discs surrounding a circular hole in a flat plate under various loading conditions /
by: Mansfield, Eric Harold, 1923-
Published: (1978)

A simplified approach to the phenomenon of wind-tunnel resonance /
by: Acum, Wilfred Ethelbert Aldred
Published: (1964)

Generalised aerodynamic forces on a T-tail oscillating harmonically in subsonic flow /
by: Davies, David Eric
Published: (1966)

The loading of helicopter rotor blades in forward flight /
by: Willmer, M. A. P.
Published: (1963)

Prediction of aerodynamic loads on rotorcraft : papers presented and discussions held at the Fluid Dynamics Panel Specialists' Meeting held at Church House, London, United Kingdom, 17-18 May 1982.
Published: (1982)

The test performance of highly loaded turbine stages designed for high preasure ratio /
by: Johnston, I. H.
Published: (1962)

The buckling of a pressurised stiffened cylinder under axial load /
by: McKenzie, K. I.
Published: (1961)

Prediction of aerodynamic loading : papers and discussions from the Fluid Dynamics Panel Symposium held at the NASA Ames Research Center, Moffett Field, California, USA, 27-29 September, 1976.
Published: (1977)

Wind and snow loading : practical studies from the Building Research Establishment.
Published: (1978)

The effect of steady tailplane lift on the oscillatory behaviour of a T-tail flutter model at high subsonic speeds /
by: Gray, R. A.
Published: (1974)

Calculation of the induced velocity field on and off the wing plane for a swept wing with given load distribution /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1973)

A free-flight investigation into the effect of body shaping on the zero-lift drag of a wing-body combination at transonic and supersonic speeds /
by: Hamilton, J. A.
Published: (1961)

Studies of air loads on man /
by: Swearingen, John J.
Published: (1963)

The pressure-drag due to blunt leading edges on two-dimensional aerofoils : at transonic and low supersonic speeds /
by: Graham, William James
Published: (1967)

Measurement of aerodynamic heating on the nose of a delta aircraft at speeds up to M = 1.65 /
by: Nethaway, J. E.
Published: (1962)

Inflated mobile lifting structures: analysis of membrane construction and design optimisation for oval planforms /
by: Brown, I. S. H.
Published: (1964)

Aircraft dynamic loads due to flow separation : Les constraintes aérodynamiques imposées aux aéronefs par le décollement de l'ecoulement.
Published: (1990)

Half-body and wing combinations in supersonic flow : a review of some principles and possibilities /
by: Goldsmith, E. L.
Published: (1968)

On the design of wing-body combinations of low zero-lift drag rise at transonic speeds /
by: Lord, W. T.
Published: (1962)