Two-dimensional normal fences on a flat plate /

The use of calibrated strain gauges for flight load determination /
by: Hovell, P. B. (Peter Burns)
Published: (1969)

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

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

737 graphite composite flight spoiler flight service evaluation : eighth report /
by: Coggeshall, Randy L.
Published: (1985)

Loads experienced in turbulence by a Central African Airways Viscount without and with cloud warning radar /
by: Bullen, Norman Ivor
Published: (1969)

Design of a symmetrical section with specified pressure distribution /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1969)

Some studies of pressure distributions on the windward surfaces of conical bodies at high supersonic speeds /
by: Akers, Arthur
Published: (1966)

The calculation of momentum thickness in a turbulent boundary layer at mach numbers up to unity /
by: Nash, John F.
Published: (1967)

Stability and control flight testing : some of the test instrumentation requirements /
by: Rose, Robert
Published: (1968)

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)

Measurements of drag, base pressure and base aerodynamic heat transfer appropriate to 8.5 semi-angle sharp cones in free flight at mach numbers from 0.8 to 3.8 /
by: Greenwood, G. H.
Published: (1967)

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

A survey of unsteady hypersonic flow problems /
by: Wood, B. M.
Published: (1966)

Wind tunnel investigation of jet interference for underwing installation of high bypass ratio engines /
by: Raney, Derek John
Published: (1969)

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)

Ground spoiler activation in flight/hard landing, ValuJet Airlines flight 558, Douglas DC-9-32, N922VV, Nashville, Tennessee, January 7, 1996 /
Published: (1996)

The accumulation of fatigue damage in aircraft materials and structures /
by: Schijve, J.
Published: (1972)

The role of heat conduction in leading edge heating theory and experiment /
by: Nonweiler, T. R. F.
Published: (1970)

Review of experimental work on stiffened plates.
Published: (1986)

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

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

Short-cowl front-fan turbojets ; friction drag and wall-jet effects on cylindrical afterbodies /
by: Green, John Edward
Published: (1969)

Report ACA.
Published: (1944)

High-speed flight propulsion systems /
Published: (1991)

Measurements at transonic speeds of the sideforce & yawing moment on various store arrangements mounted beneath a 45 swept wing-fuselage model /
by: Marsden, Philip
Published: (1967)

Low-speed theoretical and experimental aerodynamic loading on highly-swept curved-tipped wings of two thicknesses /
by: Garner, Henry Clifford
Published: (1974)

Comparison of seven wing buffet boundaries measured in wind tunnels and in flight /
by: Mabey, Dennis G.
Published: (1966)

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

Morphing aerospace vehicles and structures /
Published: (2012)

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

Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model /
by: Cox, A. P.
Published: (1967)

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)

An iterative method for calculation of the loading on a thin unswept wing /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1973)

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

Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2 [as printed, as printed]. /
by: Neale, M. C.
Published: (1967)

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