The formulation of an influence-coefficient method for determining static aeroelastic effects : and its application to a slender aircraft in symmetric flight at M = 2.2 /

Vertical accelerations due to structural vibrations of a slender aircraft flying in continuous turbulence /
by: Zbrozek, J. K.
Published: (1966)

The mixing of free axially-symmetrical jets of mach number 1.40 /
by: Johannesen, N. H.
Published: (1962)

Further results on the mixing of free axially-symmetrical jets of mach number 1.40 /
by: Johannesen, N. H.
Published: (1962)

Tables of supersonic symmetrical flow around right circular cones : with and without the addition of heat at the wave /
by: Bartlett, Ronald Stanley
Published: (1968)

Pressure-plotting and force tests at Mach numbers up to 2.8 on an uncambered slender wing of p = 1/2, s/co = 1/4 ('Handley Page Ogee') /
by: Courtney, Adrian Laurence
Published: (1964)

A numerical method for calculating the pressure due to thickness on symmetrical wings at zero incidence in supersonic flow /
by: Eldridge, Robert Henry
Published: (1968)

Oscillatory aerodynamic forces in linearised supersonic flow for arbitrary frequencies, planforms and mach numbers /
by: Allen, D. J.
Published: (1965)

The velocity potential on triangular and related wings with subsonic leading edges oscillating harmonically in supersonic flow /
by: Davies, David Eric
Published: (1961)

A new probe for the direct measurement of stagnation pressure in supersonic flow /
by: Goodyer, M. J.
Published: (1975)

Minimum drag surfaces of given lift which support two-dimensional supersonic flow fields /
by: Pike, Jack, 1937-
Published: (1968)

A form of the supersonic flow equations for an ideal gas /
by: Walkden, F.
Published: (1974)

Characteristics of high-speed wind tunnels in the United Kingdom relevant to aeroelastic-model tests /
by: Irwin, C. A. K.
Published: (1967)

Some calculations of the take-off behaviour of a slender-wing supersonic transport design constrained to follow a specified pitch-attitude time history /
by: Tomlinson, Barry Nigel
Published: (1967)

Fan supersonic flutter : prediction and test analysis /
by: Halliwell, D. G.
Published: (1977)

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

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)

The effect of combined boundary-layer suction and base bleed on the drag of a 10 degree cone at M=2.58 /
by: Goldsmith, E. L.
Published: (1970)

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)

A flight simulation study of the handling characteristics of a slender wing supersonic transport aircraft at landing approach speeds /
by: Perry, D. H. (David Howard)
Published: (1970)

Experiments with biconvex and double-wedge aerofoils in low-density, supersonic flow /
by: Rogers, E. W. E.
Published: (1970)

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

The aerodynamic forces on an oscillating two-dimensional wing in accelerated supersonic flight /
by: Davies, Danny E.
Published: (1962)

Supersonic engineering ; a symposium held at the Royal College of Advanced Technology, Salford /
Published: (1962)

Measurement of the pitching-moment derivatives for rigid tapered wings of hexagonal planform oscillating in supersonic flow /
by: Woodgate, L.
Published: (1962)

The design of compression surfaces for high supersonic speeds using conical flow fields /
by: Jones, John Glynn
Published: (1968)

Boundary layer bleed drag at supersonic speeds /
by: Goldsmith, E. L.
Published: (1968)

The transonic flow in the throat region of a two-dimensional nozzle with walls of arbitrary smooth profile /
by: Moore, A. W. (Alan William)
Published: (1967)

An experimental investigation at supersonic speeds of the characteristics of two gothic wings, one plane and one cambered /
by: Squire, Leonard Charles
Published: (1961)

An experimental assessment of the possibility of damage to leaded windows by sonic bangs /
by: Hunt, F. L.
Published: (1973)

Theory and tunnel tests of rotor blades for supersonic turbines /
by: Stratford, B. S.
Published: (1962)

Experiments at M b0 s= 4.03 on two families of pressure-plotting wing-and-half-cone combinations /
by: Rogers, E. W. E.
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)

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

A wind tunnel investigation of the longitudinal and lateral aerodynamic characteristics of a canard aircraft model ; Pt. I. Tests at M = 1.40 and M = 2.02 /
by: Watts, P. E.
Published: (1962)

A piloted simulation of the take-off of a supersonic transport aircraft with and without a take-off director /
by: Tomlinson, Barry Nigel
Published: (1969)

New design concepts for high speed air transport /
Published: (1997)