Poppet Valve Control of Throat Stability Bypass to Increase Stable Airflow Range of a Mach 2.5 Inlet with 60 Percent Internal Contraction PDF Download

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Poppet Valve Control of Throat Stability Bypass to Increase Stable Airflow Range of a Mach 2.5 Inlet with 60 Percent Internal Contraction

Poppet Valve Control of Throat Stability Bypass to Increase Stable Airflow Range of a Mach 2.5 Inlet with 60 Percent Internal Contraction PDF Author: Glenn A. Mitchell
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

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Book Description

Poppet Valve Control of Throat Stability Bypass to Increase Stable Airflow Range of a Mach 2.5 Inlet with 60 Percent Internal Contraction

Poppet Valve Control of Throat Stability Bypass to Increase Stable Airflow Range of a Mach 2.5 Inlet with 60 Percent Internal Contraction PDF Author: Glenn A. Mitchell
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

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Book Description

Poppet Valve Control of Throat Stability Bypass to Increase Stable Airflow Range of a Mach 2.5. Inlet with 60 Percent Internal Contraction

Poppet Valve Control of Throat Stability Bypass to Increase Stable Airflow Range of a Mach 2.5. Inlet with 60 Percent Internal Contraction PDF Author: Glenn A. Mitchell
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52

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Book Description
The throat of a Mach 2.5 inlet with a coldpipe termination was fitted with a stability-bypass system. System variations included several stability bypass entrance configurations. Poppet valves controlled the bypass airflow. The inlet stable airflow range achieved with each configuration was determined for both steady state conditions and internal pulse transients. Results are compared with those obtained without a stability bypass system. Transient results were also obtained for the inlet with a choke point at the diffuser exit and for the inlet with large and small stability bypass plenum volumes. Poppet valves at the stability bypass exit provided the inlet with a stable airflow range of 20 percent or greater at all static and transient conditions.

Pressure-activated Stability-bypass-control Valves to Increase the Stable Airflow Range of a Mach 2.5 Inlet with 40 Percent Internal Contraction

Pressure-activated Stability-bypass-control Valves to Increase the Stable Airflow Range of a Mach 2.5 Inlet with 40 Percent Internal Contraction PDF Author: Glenn A. Mitchell
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 108

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Aeronautical Engineering

Aeronautical Engineering PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 524

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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1056

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Throat Bypass Bleed Systems for Increasing the Stable Airflow Range of a Mach 2.50 Axisymmetric Inlet with 40 Percent Internal Contraction

Throat Bypass Bleed Systems for Increasing the Stable Airflow Range of a Mach 2.50 Axisymmetric Inlet with 40 Percent Internal Contraction PDF Author: Bobby W. Sanders
Publisher:
ISBN:
Category :
Languages : en
Pages : 87

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Government Reports Announcements & Index

Government Reports Announcements & Index PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 730

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Government Reports Annual Index

Government Reports Annual Index PDF Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 838

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Turbojet-exhaust-nozzle Secondary-airflow Pumping as an Exit Control of an Inlet-stability Bypass System for a Mach 2.5 Axisymmetric Mixed-compression Inlet

Turbojet-exhaust-nozzle Secondary-airflow Pumping as an Exit Control of an Inlet-stability Bypass System for a Mach 2.5 Axisymmetric Mixed-compression Inlet PDF Author: Bobby W. Sanders
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 88

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Cumulative Title Index to United States Public Documents, 1789-1976

Cumulative Title Index to United States Public Documents, 1789-1976 PDF Author: Daniel W. Lester
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 774

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Book Description