More tests with a variable ramp intake having 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 with variable geometry at Mach numbers from 1.7 to 2.5.
by: Brown, C. S. (Charles Scorer), et al.
Published: (1973)

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)

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

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

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)

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

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)

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)

Practical intake aerodynamic design /
Published: (1993)

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

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

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)

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

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)

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)

Intake aerodynamics /
Published: (1999)

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)

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)

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)

An experimental investigation of the two-dimensional wall jet /
by: Whitelaw, James H.
Published: (1967)

Airframe/propulsion interference.
Published: (1975)

The local pressure field of turbulent jets /
by: Davies, Peter Owen Alfred Lawe
Published: (1968)

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

An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0 /
by: Re, Richard J.
Published: (1976)

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

The use of air injection to prevent separation of the turbulent boundary layer in supersonic flow /
by: Peake, D. J.
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)

Noise suppression by an acoustically treated three-ring inlet on a TF-34 engine /
by: Minner, Gene L., et al.
Published: (1976)

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

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /
by: Trefny, Charles J., et al.
Published: (1986)