Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2 /

Wind-tunnel tests on a rectangular, twin-duct, variable-geometry air intake : at supersonic speeds /
by: Dobson, M. D.
Published: (1967)

An experimental investigation of the flow through inclined circular tubes at a mach number of 4.0,
by: Roe, P. L.
Published: (1966)

Measurement of the internal performance of a rectangular air-intake at Mach number of 0.9 /
by: Brown, C. S. (Aerospace engineer), et al.
Published: (1976)

Measurement of the internal performance of a rectangular air intake with variable geometry at Mach numbers from 1.7 to 2.5.
by: Brown, C. S. (Charles Scorer), et al.
Published: (1973)

The external drag of fuselage side intakes : rectangular intakes with compression surfaces vertical /
by: Dobson, M. D.
Published: (1974)

The performance of some axisymmetric isentropic centrebody intakes designed for mach numbers of 2.48 and 3.27 /
by: Goldsmith, E. L.
Published: (1969)

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

A supersonic tunnel design for testing engine intakes /
by: Staniforth, R.
Published: (1961)

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

Air intake problems in supersonic propulsion ; invited papers presented at the 11th AGARD Combustion and Propulsion Panel meeting, Paris, December 1956 /
Published: (1958)

Thrust performance of isolated two dimension suppressed plug nozzles with and without ejectors at mach numbers from 0 to 0.45 /
by: Harrington, Douglas E., et al.
Published: (1976)

Intake aerodynamics /
Published: (1999)

The effect of internal contraction, initial rate of subsonic diffusion, and cowl and contrebody shape on the pressure recovery of a conical-centrebody intake at supersonic speeds /
by: Goldsmith, E. L.
Published: (1962)

Practical intake aerodynamic design /
Published: (1993)

On the static performance of two-dimensional intakes with momentum injection in the form of boundary-layer control by blowing /
by: Gregory, Nigel
Published: (1971)

Boundary-layer interaction effects in intakes with particular reference to those designed for dual subsonic and supersonic performance /
by: Seddon, J.
Published: (1970)

Analysis of experimental results of the inlet for the NASA hypersonic research engine aerothermodynamic integration model /
by: Andrews, Earl H., et al.
Published: (1976)

Computational design and optimization of supersonic intakes /
by: Sandhu, Jatinder Pal Singh, et al.
Published: (2025)

Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction /
by: Shaw, Robert J. (Robert Joseph), 1946-, et al.
Published: (1976)

A theoretical and experimental investigation of the external-flow, jet-augmented flap /
by: Ashill, P. R.
Published: (1975)

Intake aerodynamics /
Published: (1999)

An experimental investigation of the two-dimensional wall jet /
by: Whitelaw, James H.
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)

Aerodynamic performance of flared fan nozzles used as inlets /
by: Dietrich, Donald A., et al.
Published: (1976)

Supersonic inlets /
by: Faro, Ione D. V.
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 performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /
by: Trefny, Charles J., et al.
Published: (1986)

Heat transfer in the vicinity of a 15° compression corner at Mach numbers from 2.5 to 4.4 /
by: Hastings, R. C., et al.
Published: (1967)

Measurement of the internal performance of a rectangular air intake mounted on a fuselage at mach numbers from 1.6 to 2.
by: Brown, C. S. (Aerospace engineer), et al.
Published: (1974)

Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack /
by: Latham, Eldon A.
Published: (1976)

Results of a series of wind tunnel tests on the Victor B. Mk. 2 aircraft and a comparison with drag estimates and full scale flight data /
by: Simper, J. I. (Aircraft researcher)
Published: (1974)

Intake research facilities manual : final report, May 1985 /
Published: (1985)

Hydraulic design of short intake for deep outlet works /
Published: (1980)

Free-flight model measurements of the dynamic stability of a supersonic strike aircraft (TSR2) /
by: Hunt, G. K.
Published: (1967)

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

Further analysis of TSR.2 flights through turbulence /
by: Saunders, T. B.
Published: (1968)