Results and analysis of pressure measurements on two isolated slender wings and slender wing-body combinations at supersonic speeds /

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

A simple flexible supersonic wind tunnell nozzle for the rapid and accurate variation of flow mach number /
by: Pierce, D.
Published: (1967)

Experimental effects of wing location on wing-body pressures at supersonic speeds /
by: Allen, Jerry M., et al.
Published: (1993)

Measurements of buffeting on slender wing models /
by: Mabey, Dennis G.
Published: (1967)

A technique for the wind tunnel simulation of store release at high speeds /
by: Beecham, L. J.
Published: (1966)

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

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

Supersonic flutter derivatives for a series of swept and cropped delta wings /
by: Harris, G. Z.
Published: (1967)

The correlation and prediction of pressure distributions on compression surfaces of sharp-edged conical bodies at high supersonic speeds /
by: Larcombe, M. J.
Published: (1969)

The response times of typical transducer-tube configurations for the measurement of pressures in high-speed wind tunnels /
by: Larcombe, M. J.
Published: (1966)

Exploratory studies on the sublimation of slender camphor and naphthalene models in a supersonic wind-tunnel /
by: Charwat, A. F.
Published: (1968)

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)

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)

Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model /
by: Ray, Edward J., et al.
Published: (1966)

An analogue computer for on-line correction of wind-tunnel force and moment data /
by: Pecover, B. E.
Published: (1967)

A method of correlating the ground effects on the longitudinal characteristics of slender wings /
by: Kirkpatrick, David L. I.
Published: (1970)

Pressure probe designs for dynamic pressure measurements in a supersonic flow field /
by: Porro, A. Robert
Published: (2001)

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

Characteristics of aft-mounted all-moving rectangular control surfaces on a slender cruciform model at mach numbers from 0.6 to 2.8 /
by: Winter, Kenneth George
Published: (1968)

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 dynamic stability derivatives of a slender wing : a comparison of theory with free-flight model tests at near-zero lift, M = 0.8 to 2.4 /
by: Turner, K. J.
Published: (1968)

Camber effects on the non-linear lift of slender wings with sharp leading edges /
by: Squire, Leonard Charles
Published: (1967)

Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /
by: Hallissy, James B.
Published: (1989)

Measurement of the internal drag of air breathing installations on slender wing-body combinations at supersonic speeds /
by: Britton, J. W.
Published: (1967)

The accuracy of pressure transducers when used in short-duration wind-tunnel facilities /
by: Pennelegion, L.
Published: (1967)

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

Supersonic interference flow along the corner of intersecting wedges /
by: Charwat, A. F.
Published: (1966)

Tests on an engine installation for a slender gothic wing at M-1.82 /
by: Griffiths, R. T.
Published: (1967)

The 8 x 6 supersonic wind tunnel.
Published: (1994)

Interim report on low-speed flight tests of a slender-wing research aircraft (Handley Page H. P. 115) /
by: Bisgood, P. L.
Published: (1966)

Tests at transonic speeds on wings with wedge sections and sweep varying between 0 and 60 /
by: Rogers, E. W. E.
Published: (1963)

Guided weapons aerodynamic study: force and moment measurements on some monoplane and cruciform slender wing-body combinations at M-4.0 /
by: Roe, P. 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)

Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel /
by: Castner, Raymond S.
Published: (2013)

Investigation of the normal force characteristics of slender delta wings with various rhombic cross-sections in subsonic conical flow /
by: Kirkpatrick, David L. I.
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)