Servosystem design of a high-response slotted- plate overboard bypass valve for a supersonic inlet | ORKG Ask

We use cookies to provide a better user experience.

Data Protection

Related items

Servosystem design of a high-response slotted-plate overboard bypass valve for a supersonic inlet /

Neiner, George H.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1970

The servosystem design of a high-response airflow bypass valving system for supersonic mixed-compres...

Improved design of a high response slotted plate overboard bypass valve for supersonic inlets

Hiller, K. W.
Webb, J. A., Jr.
Mehmed, O.

June 1973

The electrohydraulically actuated slotted-plate bypass valve used to control the position of the nor...

Analysis of a stability valve system for extending the dynamic range of a supersonic inlet

Dustin, M. O.
Webb, J. A., Jr.

May 1975

A stability valve system designed for a full-scale, flight, supersonic, mixed-compression inlet was ...

Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds /

Leiss, Abraham.
Kouyoumjian, Walter J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1958

A method is presented to design a supersonic inlet that will match turbojet-engine air mass-flow req...

Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds /

Leiss, Abraham.
Kouyoumjian, Walter J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1958

A method is presented to design a supersonic inlet that will match turbojet-engine air mass-flow req...