A flight simulation study of the handling characteristics of a slender wing supersonic transport aircraft at landing approach speeds /

The longitudinal response of a flexible slender aircraft to random trubulence /
by: Huntley, E.
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)

A flight simulator for research into aircraft handling characteristics /
by: Perry, D. H. (David Howard)
Published: (1969)

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

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)

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)

A simulation of the low speed handling of the BAC 221 slender-wing research aircraft /
by: Wilcock, Trevor
Published: (1971)

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 /
by: Taylor, A. S.
Published: (1969)

A piloted simulator study of a slender-wing research aircraft (HP 115) /
by: McPherson, A.
Published: (1970)

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

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)

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)

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

Supersonic flight ; the story of the Bell X-1 and Douglas D-558 /
by: Hallion, Richard, 1948-
Published: (1972)

Forty years of supersonic flight : open house '87 Edwards AFB.
Published: (1987)

Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds /
by: Carlson, Harry W., et al.
Published: (1980)

Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1966)

A Pre-flight simulation of the B.A.C. 221 slender-wing research aircraft /
by: McPherson, A.
Published: (1969)

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

An experimental and theoretical comparison at M=4 of the lift-to-drag ratio of some possible aircraft shapes /
by: Brown, C. S. (Charles Scorer)
Published: (1969)

Evaluation of high-speed civil transport handling qualities criteria with supersonic flight data /
by: Cox, Timothy H., et al.
Published: (1997)

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)

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)

Some problems in the automatic control and stability of supersonic transport aircraft /
by: Ruggles, R.
Published: (1970)

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)

An extensive theoretical study of the ability of slender-wing aircraft to perform sidestep manoeuvres at approach speeds /
by: Tomlinson, Barry Nigel
Published: (1964)

U.S. supersonic commercial aircraft : assessing NASA's high speed research program /
Published: (1997)

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

Anticollision lights for the supersonic transport (SST) /
by: Gerathewohl, Siegfried J. (Siegfried Johannes), 1909-
Published: (1970)

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

Design of a supersonic nozzle /
by: McCabe, A.
Published: (1967)

The performance of supersonic turbine nozzles /
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)

Further piloted simulation studies of the handling characteristics of a slender-wing supersonic transport aircraft during approach and landing.
by: Tomlinson, B. N.
Published: (1871)

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