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Leakage and secondary flows in compressor cascades

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Series: ARC R&M 3483 : 1965Edition: Language: English Publication details: London ; Her Majesty's Stationary Office ; 1965Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: DARC R&M 3483 : 1965.

Flight measurement of the elevator and aileron hinge-moment derivatives of the fairey delta 2 aircraft upto a Mach number of 1.6 and comparisons with wind-tunnel results

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Series: ARC R&M 3485 : 1965Edition: Language: English Publication details: London ; Her Majesty's Stationary Office ; 1965Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: DARC R&M 3485 : 1965.

Calculation of the spanwide loading of sweptback wings with flaps or all-moving tips at subsonic speeds

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Series: ARC R&M 3487 : 1965Edition: Language: English Publication details: London ; Her Majesty's Stationary Office ; 1965Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: DARC R&M 3487 : 1965.

Some calculations of the take-off behavior of a slender-wing supersonic transport design constrained to follow a specified pitch-attitude time history

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Series: ARC R&M 3493 : 1965Edition: Language: English Publication details: London ; Her Majesty's Stationary Office ; 1965Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: DARC R&M 3493 : 1965.

Wind-tunnel tests on a nacelle fitted with two lifting fans in tandem

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Series: ARC R&M 3494 : 1965Edition: Language: English Publication details: London ; Her Majesty's Stationary Office ; 1965Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: DARC R&M 3494 : 1965.

Flow produced by interaction of a turbulent boundary layer with a normal shock wave of strength sufficient to cause separation

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Series: ARC R&M 3502 : 1960Edition: Language: English Publication details: London ; Her Majesty's Stationary Office ; 1960Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: DARC R&M 3502 : 1960.

Linearized flow field of a relaxing gas through a non-uniform channel and in a jet at supersonic speeds

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Series: ARC R&M 3504 : 1964Edition: Language: English Publication details: London ; Her Majesty's Stationary Office ; 1964Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: DARC R&M 3504 : 1964.

Steady flow in the boundary layer near the surface of a cylinder in a stream

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Series: ARC R&M 1632 : 1935Edition: Language: English Publication details: London ; Her Majesty's Stationary Office ; 1935Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: DARC R&M 1632 : 1935.

Calculation of the warp to produce a given load and the pressure due to a given thickness on thin slender wings in supersonic flow

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Series: ARC R&M 3471 : 1965Edition: Language: English Publication details: London ; Her Majesty's Stationary Office ; 1965Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: DARC R&M 3471 : 1965.

Fatigue test results and analysis of 42 piston provost wings

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Series: ARC R&M 3474 : 1965Edition: Language: English Publication details: London ; Her Majesty's Stationary Office ; 1965Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: DARC R&M 3474 : 1965.

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