The performance of conical convergent-divergent nozzles of area ratios 2.44 and 2.14 in external flow /

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)

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

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

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

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

Supersonic wind tunnel nozzles : a selected, annotated bibliography to aid in the development of quiet wind tunnel technology /
by: Wolf, Stephen W. D.
Published: (1990)

Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air /
by: Scallion, W. I.
Published: (1991)

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

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

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)

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

Exhaust nozzle plume effects on sonic boom test results for isolated nozzles /
by: Castner, Raymond S.
Published: (2011)

Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /
by: Berrier, Bobby L., et al.
Published: (1980)

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

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)

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)

Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles /
by: Yetter, Jeffery A., et al.
Published: (1980)

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

Estimation of surface pressures from observed shock-wave envelopes surrounding conical bodies at M = 4.0 /
by: Larcombe, M. J.
Published: (1970)

The effect of a cylindrical shroud on the performance of a stationary convergent nozzle /
by: Reid, J.
Published: (1963)

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

Analysis and design of optimized truncated scarfed nozzles subject to external flow effects /
by: Shyne, Rickey J.
Published: (1990)

Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf /
by: Lamb, Milton, et al.
Published: (1996)

A convergent nozzle for the standardisation of thrust-rig measurements /
by: Herbert, M. V.
Published: (1969)

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 study of efficient means of solving transonic flow problems /
by: Trevino, John, 1959-
Published: (1983)

Characteristics of sewage-sprinkler nozzles /
by: Wiley, Ralph Benjamin
Published: (1925)

Cracking in pressurizer safety and relief nozzles and in surge line nozzle.
Published: (2004)

Converging-diverging nozzle thruster code for nuclear or chemical rocket performance computations /
by: Juhasz, Albert J.
Published: (2019)

Studies of flow fields created by vertical and inclined jets when stationary or moving over a horizontal surface /
by: Abbott, W. A.
Published: (1967)

Coefficients of discharge of sewage-sprinkler nozzles /
by: Greve, Frederick William, 1885-
Published: (1919)

The effects of base bleed on plug nozzles /
by: Reid, J.
Published: (1967)

Analytical and experimental studies of sound suppressor components for NASA rocket engine test stands /
Published: (1967)

An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization /
by: Axdahl, Erik L.
Published: (2015)

Gas flow in nozzles /
by: Pirumov, Ul
Published: (1986)

Research on flow nozzles /
Published: (1948)