Supersonic flutter derivatives for a series of swept and cropped delta wings /

The pressure distribution at zero lift on a slender delta wing at transonic speeds /
by: Firmin, Michael Charles Peter, 1929-
Published: (1968)

Calculation of subsonic flutter derivatives for an arrowhead wing with control surfaces /
by: Lehrian, Doris E.
Published: (1969)

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)

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

The lift and drag characteristics of caret wings at Mach numbers between 5 and 10 /
by: Collingbourne, J. R.
Published: (1967)

Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers /
by: Blair, A. B.
Published: (1976)

Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds /
by: Shaw, M. M.
Published: (1967)

The subcritical response and flutter of a swept-wing model /
by: Irwin, C. A. K.
Published: (1968)

Gun tunnel measurements of lift : drag and pitching moment on a 20 p0 scone, a flat delta and caret delta wing at a mach number of 8.3 /
by: Opatowski, T.
Published: (1967)

Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls /
by: Isaacs, Donald
Published: (1969)

Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons /
by: Butler, S. F. J.
Published: (1966)

Measurements of the pitching-moment derivatives on a sharp-edged delta wing in incompressible flow /
by: Woodgate, L.
Published: (1964)

Measurements of skin friction on a cambered delta wing at supersonic speeds /
by: Winter, Kenneth George
Published: (1967)

Some possible effects of transonic speeds on wing-aileron flutter /
by: Broadbent, E. G.
Published: (1962)

The subcritical response and flutter of a slender wing model aircraft /
by: Payen, D. B.
Published: (1969)

Low-speed wind-tunnel experiments on a series of sharp-edged delta wings /
by: Earnshaw, P. B.
Published: (1966)

Flutter characteristics of a wing carrying a flexibly mounted mass /
by: Gaukroger, D. R. (Donald Richard)
Published: (1963)

Measurements of the direct pitching oscillation derivatives for three cropped delta and three arrowhead planforms at subsonic and transonic speeds /
by: Miles, C. J. W.
Published: (1965)

Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges /
by: Vigneron, Yvon Clovis
Published: (1978)

Analysis of the static pressure distribution on a Delta wing in subsonic flow /
by: Kirkpatrick, David L. I.
Published: (1970)

Introduction to flutter of winged aircraft : December 09-13, 1991 /
Published: (1992)

The longitudinal characteristics of three slender 'mild ogee' wings at mach numbers from 0.4 to 2.0 /
by: Mabey, Dennis G.
Published: (1968)

Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16 /
by: Wood, Richard M., et al.
Published: (1985)

Analysis of the zero-lift wave drag measured on delta wings /
by: Weber, J.
Published: (1978)

Wing theory in supersonic flow /
by: Carafoli, Elie
Published: (1969)

Low-speed wind-tunnel measurements of the lift, drag, and pitching moment of a series of cropped delta wings /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1974)

Pressure measurements on a model delta wing undergoing oscillatory deformation /
by: Lambourne, N. C.
Published: (1972)

Specialists meeting on Wing-with-stores Flutter : papers presented at the 39th meeting of the Structures and Materials Panel in Munich, Germany, 6-12 October, 1974.
Published: (1975)

Use of camber and twist to produce low-drag delta or swept-back wings, without leading-edge singularities, at supersonic speeds /
by: Roper, G. M.
Published: (1961)

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

Exploratory investigation of the effects of blowing from the leading edge of a delta wing /
by: Trebble, W. J. G.
Published: (1968)

A use of arbitrary modes in control-surface flutter investigations /
by: Niblett, Ll. T.
Published: (1967)

Flow past conically-cambered slender delta wings with leading-edge separation /
by: Barsby, J. E.
Published: (1974)

Calculations of the effect of blowing from the leading edges of a slender delta wing /
by: Barsby, J. E.
Published: (1972)

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

Co-ordinated experimental and theoretical research on the oscillatory airforces for selected planforms at subsonic and supersonic speeds /
by: Woodcock, David Leon, 1922-
Published: (1969)