A simple flexible supersonic wind tunnell nozzle for the rapid and accurate variation of flow mach number /

The performance of conical convergent-divergent nozzles of area ratios 2.44 and 2.14 in external flow /
by: Golesworthy, G. T.
Published: (1967)

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

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

The performance of supersonic turbine nozzles /
by: Stratford, B. S.
Published: (1962)

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

An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations /
by: Roberts, J. B. (Writer on aerodynamics)
Published: (1967)

A theoretical study of annular supersonic nozzles /
by: Lord, W. T.
Published: (1961)

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

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

Design and operation of intermittent supersonic wind tunnels /
by: Ferri, Antonio, 1912-
Published: (1954)

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)

Boundary-layer separation in supersonic propelling nozzles /
by: Herbert, M. V.
Published: (1966)

An experiment on aerodynamic nozzles at M = 2 /
by: Reid, J.
Published: (1964)

Supersonic inlet test for a quiet supersonic transport technology demonstrator in the NASA Glenn 8-by 6-foot supersonic wind tunnel /
by: Castner, Raymond S., et al.
Published: (2018)

Transonic throat flow in radial or nearly radial supersonic nozzles /
by: Carroll, Bruce Frederick, 1960-
Published: (1984)

Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles /
by: Castner, Raymond S.
Published: (2010)

NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 /
by: Wolf, Stephen W. D., et al.
Published: (1997)

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

The effect of a central jet on the base pressure of a cylindrical after-body in a supersonic stream /
by: Reid, J.
Published: (1961)

High-speed wind tunnel testing.
by: Pope, Alan, 1913-
Published: (1965)

A graphite resistance heater for a hypersonic wind tunnel using nitrogen /
Published: (1961)

Measurements of fluctuating pressures in 8- by 6-foot supersonic wind tunnel for Mach number range of 0.56 to 2.07 /
by: Karabinus, Raymond J., et al.
Published: (1970)

Nozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel /
by: Durston, D. A.
Published: (2018)

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

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01 /
by: Foster, Gerald V.
Published: (1959)

The transonic flow in the throat region of a two-dimensional nozzle with walls of arbitrary smooth profile /
by: Moore, A. W. (Alan William)
Published: (1967)

Measurements in a three-dimensional turbulent boundary layer in supersonic flow /
by: Hall, Michael George
Published: (1968)

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)

Further tests with a variable ramp intake having a design Mach number of 2.2 /
by: Neale, M. C.
Published: (1966)

Some comments on the conditions in a local supersonic flow region /
by: Moulden, Trevor H.
Published: (1968)

Flow quality survey of the 8-by 6-foot supersonic wind tunnel (2015 test) prior to the 9-by 15-foot low-speed wind tunnel acoustic improvement modifications /
by: Johnson, Aaron M.
Published: (2018)

Summary of the 2017 blockage test in the 10- by 10-foot supersonic wind tunnel /
by: Pastor-Barsi, Christine, 1982-, et al.
Published: (2018)

An experimental device for generating high frequency perturbations in supersonic wind tunnels /
by: Melcher, Kevin J., et al.
Published: (1996)

NASA Glenn 1-by 1-foot supersonic wind tunnel user manual /
by: Seablom, Kirk D.
Published: (1999)

Supersonic laminar boundary layers on cones /
by: Cooke, J. C. (John Caister)
Published: (1969)

1-by 1- foot supersonic wind tunnel sidewall flowfield compression plate study /
by: Peters, Christopher J. (Christopher John), et al.
Published: (2020)