A study of dynamic aeroelastic effects on the stability control and gust response of a slender delta aircraft /

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

Gust loads on aircraft : concepts and applications /
by: Hoblit, Frederic M.
Published: (1988)

Computer programmes to calculate the response of flexible aircraft to gusts and control movements /
by: Mitchell, C. G. B.
Published: (1967)

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

Gusts, discrete and indiscrete /
by: Bullen, Norman Ivor
Published: (1970)

Theoretical analysis of a gust alleviator used on a 'Lancaster' aircraft and comparison with experiment /
by: Zbrożek, J. K.
Published: (1963)

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

A review of counting accelerometer data on aircraft gust loads /
by: Bullen, Norman Ivor
Published: (1967)

Atmospheric gusts ; a review of the results of some recent R.A.E. research /
by: Burnham, Jack
Published: (1970)

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)

Some properties of a five-parameter bivariate probability distribution /
by: Tubbs, J. D.
Published: (1983)

Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results /
by: Rose, Robert
Published: (1969)

A momentum analysis of lifting surfaces in inviscid supersonic flow /
by: Roe, P. L.
Published: (1969)

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

Accuracy of downwash evaluation by Multhopp's lifting-surface theory /
by: Garner, Henry Clifford
Published: (1966)

Comparison of three methods for the evaluation of subsonic lifting-surface theory /
by: Garner, Henry Clifford
Published: (1969)

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)

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

Survey of applications of active control technology for gust alleviation and new challenges for lighter-weight aircraft /
by: Regan, Christopher D., et al.
Published: (2012)

Theory of lifting surfaces oscillating at general frequencies in a subsonic stream /
by: Acum, Wilfred Ethelbert Aldred
Published: (1969)

Active spanwise lift control : a distributed parameter approach /
by: Dias, Joaquim Neto, et al.
Published: (2020)

Variable stability and control tests on the S.C.1 aircraft in jet-borne flight, with particular reference to desirable VTOL flying qualities /
by: Illingworth, J. K. B.
Published: (1969)

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

Algol 60 programme for Multhopp's low-frequency subsonic lifting-surface theory /
by: Garner, Henry Clifford
Published: (1968)

Comparative theoretical calculations of forces on oscillating wings through the transonic speed range /
by: Garner, Henry Clifford
Published: (1969)

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

Experimental investigation of the effect of trailing-edge sweepback on the subsonic longitudinal characteristics of slender wings, by D. L. I. Kirkpatrick and A. G. Hepworth.
by: Kirkpatrick, David L. I.
Published: (1970)

The lift and stalling characteristics of a 35 deg. swept back wing designed to have identical chordwise pressure distributions at all spanwise stations when near maximum lift /
by: Woodward, D. S.
Published: (1973)

An approximate treatment of the stability of a towed unbanked object in a condition of zero lift /
by: Hopkin, H. R.
Published: (1971)

The flutter and stability of undamped systems /
by: Done, George Taylor Sutton
Published: (1968)

A small aircraft gust-probe system /
by: Gilmer, R. O., et al.
Published: (1977)

Further experimental investigation of the characteristics of cambered gothic wings at Mach numbers from 0.4 to 2.0 /
by: Squire, Leonard Charles
Published: (1963)

Application of statistical theory of extreme values to gust-load problems : progress report for January - March 1952 /
Published: (1952)

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

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)