The accuracy of pressure transducers when used in short-duration wind-tunnel facilities /

Results and analysis of pressure measurements on two isolated slender wings and slender wing-body combinations at supersonic speeds /
by: Fellows, K. A.
Published: (1970)

Optical-fiber velocity and pressure transducers /
by: Zhilin, V. G. (Vi͡acheslav Gavrilovich)
Published: (1990)

Performance of the low pressure differential and absolute digiquartz pressure transducers /
by: Banaszek, A. D.
Published: (1985)

Automatic pressure measuring systems used with high-speed wind tunnels.
Published: (1955)

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

Wall corrections to longitudinal components measured on wind-tunnel models with tails /
by: Lovell, D. A.
Published: (1969)

A note on the design and construction of a low-pressure calibrator and a comparison with shock-tube and static calibration methods /
by: Pallant, R. J.
Published: (1967)

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

Super VC 10 cruise drag-A wind-tunnel investigation /
by: Taylor, C. R.
Published: (1970)

An ejector-driven wind tunnel for the generation of turbulent flows with arbitrary mean velocity profile /
by: Teunissen, H. W.
Published: (1969)

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

A method for correcting measurements of the heat transfer factor through the skin of a wind tunnel model /
by: Piggott, Brian Alexander Martin
Published: (1966)

Finite difference solutions for an unsteady interference parameter in slotted wind tunnels /
by: Rushton, K. R.
Published: (1969)

The new system for controlling the attitude and motivator deflections of a model in the R.A.E. No. 19 wind tunnel /
by: Pecover, B. E.
Published: (1968)

Wind tunnel studies of buildings and structures /
Published: (1998)

A study on the running times in reflected shock tunnels /
by: Ackroyd, J. A. D.
Published: (1967)

Some flight and wind-tunnel longitudinal stability measurements on the BAC slender-wing aircraft /
by: Barnes, C. S.
Published: (1970)

Determination of stagnation temperatures in the R.A.R.D.E. hypersonic gun tunnel from streak camera measurements of flow velocity /
by: Bowman, J. E.
Published: (1967)

Nitrogen condensation in the R.A.R.D.E. hypersonic gun tunnel /
by: Bowman, J. E.
Published: (1967)

Indwelling and implantable pressure transducers : based on workshop held in Cleveland, Ohio on December 4 and 5, 1975, sponsored by the Biotechnology Resources Branch (RR-00857) and the National Institute of General Medical Sciences (GM-14267) of the National Institutes of Health /
Published: (1977)

Low-speed wind-tunnel tests of a number of fin configurations on a flat-plate gothic wing of unit aspect ratio /
by: Peckham, D. H.
Published: (1969)

Some exploratory tests on a two-dimensional blowncylinder model in R.A.E. 2 ft. x 1 1/2 ft. transonic-wind tunnel /
by: Jones, A. F.
Published: (1967)

Experimental investigation of means for reducing the response of pressure transducers to thermal transients /

Bulk compressibility effects in the R.A.R.D.E. no. 3 hypersonic gun tunnel /
by: Clayden, W. A.
Published: (1966)

Wind tunnel model studies of buildings and structures /
Published: (1987)

A short time response stagnation temperature probe /
by: East, R. A.
Published: (1967)

Pressure sensors : selection and application /
by: Tandeske, Duane, 1937-
Published: (1991)

Wind tunnels : proposal for a new national wind tunnel complex /
by: Radzanowski, David P.
Published: (1995)

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)

Subsonic tests in free molecule flow on impact tube pressure probes having a wide range of tube lengths at angles of attack up to 90 ̊ /
by: Hughes, Peter C. (Peter Carlisle), 1940-
Published: (1965)

Tests at a mach number of 2.0 on a rectangular twin-duct air intake with variable geometry : situated in the flow field of a slender wing /
by: Dobson, M. D.
Published: (1970)

Low-speed tunnel tests of an aspect-ratio 9 jet-flap model, with ground simulation by moving-belt rig /
by: Butler, S. F. J.
Published: (1966)

Industrial pressure, level, and density measurement /
by: Gillum, Donald R.
Published: (2009)

The designers' handbook of pressure-sensing devices /
by: Lyons, Jerry L.
Published: (1980)

Use of submersible pressure transducers in water-resources investigations /
Published: (2004)

The change in shock-tunnel tailoring Mach number due to driver gas mixtures of helium and nitrogen /
by: Pennelegion, L.
Published: (1965)