Effect of several porous casing treatments on stall limit and on overall performance of an axial-flow compressor rotor /

Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, respectively, and with design pressure ratio of 2.05 /

Moore, Royce D.
Reid, Lonnie.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."April 1982"--Cover."Lewis Research Center."Mode of access: Internet

Stall Margin Improvement in a Centrifugal Compressor through Inducer Casing Treatment

V. V. N. K. Satish Koyyalamudi
Quamber H. Nagpurwala

January 2016

The increasing trend of high stage pressure ratio with increased aerodynamic loading has led to redu...

Assessment of the Self-Recirculating Casing Treatment Concept to Axial Compressors

Vishwas Iyengar
Lakshmi N. Sankar

January 2015

Performance characteristics of a transonic axial flow compressor called NASA Rotor 67 have been anal...

Effect of casing treatment on overall and blade-element performance of a compressor rotor /

Moore, Royce D.
Blade, Robert J.
Kovich, George.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by Lewis Research Center."November 1971."N72-10025.Includes bibliographical references (p. ...

Stalled and stall-free performance of axial-flow compressor stage with three inlet-guide-vane and stator-blade settings /

Urasek, Donald C.
Cunnan, Walter S.
Steinke, Ronald J.
Lewis Research Center.

January 1977

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ac...

Effect of slotted casing treatment on performance of a multistage compressor /

Moss, John E.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ac...

Effect of several porous casing treatments on stall limit and on overall performance of an axial flow compressor rotor

Heidelberg, L. J.
Lewis, G. W., Jr.
Osborn, W. M.

November 1971

Several geometrically different porous casings were tested with an axial-flow compressor rotor to de...

Research on rotating stall in axial flow compressors.

Moore, F. K.
Armed Services Technical Information Agency (U.S.)
Wright Air Development Center.

"January 1959."Includes bibliographical references (p. 16).Mode of access: Internet

Experimental assessment on effect of lower porosities of bend skewed casing treatment on the performance of high speed compressor stage with tip critical rotor characteristics

Alone, DB
Kumar, SS
Shobhavathy, MT
Mudipalli, JRR
Pradeep, AM
Ramamurthy, S
Iyengar, VS

January 2017

Development of casing treatment geometries which will enhance the stable operating envelope of the c...

NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results /

Schulze, Wallace M.
Ashby, George C.
Erwin, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

A typical axial-flow compressor rotor using NACA 65-series compressor blades was tested at low speed...

Understanding of an effect of plenum volume of a low porosity bend skewed casing treatment on the performance of single-stage transonic axial flow compressor

Pitroda, DP
Alone,, DB
Choksi, HS

January 2021

The present study intends to improve the performance of transonic axial flow compressor stage and it...

Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.78, respectively, and with design pressure ratio of 1.82 /

Moore, Royce D.
Reid, Lonnie.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."Lewis Research Center.""February 1982"--Cover.Includes bibliographical references....

Effect of damper on overall and blade-element performance of a compressor rotor having a tip speed of 1151 feet per second and an aspect ratio of 3.6 /

Lewis, George W., Jr.
Hager, Roy D.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...

Effect of casing treatment on overall and blade element performance of a compressor rotor

Kovich, G.
Moore, R. D.
Blade, R. J.

November 1971

An axial flow compressor rotor was tested at design speed with six different casing treatments acros...

Effect of inducer inlet and diffuser throat areas on performance of a low pressure ratio sweptback centrifugal compressor /

Klassen, Hugh A.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ac...

Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, respectively, and with design pressure ratio of 2.05 /

Moore, Royce D.
Reid, Lonnie.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."April 1982"--Cover."Lewis Research Center."Mode of access: Internet

Stall Margin Improvement in a Centrifugal Compressor through Inducer Casing Treatment

V. V. N. K. Satish Koyyalamudi
Quamber H. Nagpurwala

January 2016

The increasing trend of high stage pressure ratio with increased aerodynamic loading has led to redu...

Assessment of the Self-Recirculating Casing Treatment Concept to Axial Compressors

Vishwas Iyengar
Lakshmi N. Sankar

January 2015

Performance characteristics of a transonic axial flow compressor called NASA Rotor 67 have been anal...

Effect of casing treatment on overall and blade-element performance of a compressor rotor /

Moore, Royce D.
Blade, Robert J.
Kovich, George.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by Lewis Research Center."November 1971."N72-10025.Includes bibliographical references (p. ...

Stalled and stall-free performance of axial-flow compressor stage with three inlet-guide-vane and stator-blade settings /

Urasek, Donald C.
Cunnan, Walter S.
Steinke, Ronald J.
Lewis Research Center.

January 1977

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ac...

Effect of slotted casing treatment on performance of a multistage compressor /

Moss, John E.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ac...

Effect of several porous casing treatments on stall limit and on overall performance of an axial flow compressor rotor

Heidelberg, L. J.
Lewis, G. W., Jr.
Osborn, W. M.

November 1971

Several geometrically different porous casings were tested with an axial-flow compressor rotor to de...

Research on rotating stall in axial flow compressors.

Moore, F. K.
Armed Services Technical Information Agency (U.S.)
Wright Air Development Center.

"January 1959."Includes bibliographical references (p. 16).Mode of access: Internet

Experimental assessment on effect of lower porosities of bend skewed casing treatment on the performance of high speed compressor stage with tip critical rotor characteristics

Alone, DB
Kumar, SS
Shobhavathy, MT
Mudipalli, JRR
Pradeep, AM
Ramamurthy, S
Iyengar, VS

January 2017

Development of casing treatment geometries which will enhance the stable operating envelope of the c...

NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results /

Schulze, Wallace M.
Ashby, George C.
Erwin, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

A typical axial-flow compressor rotor using NACA 65-series compressor blades was tested at low speed...

Understanding of an effect of plenum volume of a low porosity bend skewed casing treatment on the performance of single-stage transonic axial flow compressor

Pitroda, DP
Alone,, DB
Choksi, HS

January 2021

The present study intends to improve the performance of transonic axial flow compressor stage and it...

Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.78, respectively, and with design pressure ratio of 1.82 /

Moore, Royce D.
Reid, Lonnie.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."Lewis Research Center.""February 1982"--Cover.Includes bibliographical references....

Effect of damper on overall and blade-element performance of a compressor rotor having a tip speed of 1151 feet per second and an aspect ratio of 3.6 /

Lewis, George W., Jr.
Hager, Roy D.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...

Effect of casing treatment on overall and blade element performance of a compressor rotor

Kovich, G.
Moore, R. D.
Blade, R. J.

November 1971

An axial flow compressor rotor was tested at design speed with six different casing treatments acros...

Effect of inducer inlet and diffuser throat areas on performance of a low pressure ratio sweptback centrifugal compressor /

Klassen, Hugh A.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ac...

Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, respectively, and with design pressure ratio of 2.05 /

Moore, Royce D.
Reid, Lonnie.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."April 1982"--Cover."Lewis Research Center."Mode of access: Internet

Stall Margin Improvement in a Centrifugal Compressor through Inducer Casing Treatment

V. V. N. K. Satish Koyyalamudi
Quamber H. Nagpurwala

January 2016

The increasing trend of high stage pressure ratio with increased aerodynamic loading has led to redu...

Assessment of the Self-Recirculating Casing Treatment Concept to Axial Compressors

Vishwas Iyengar
Lakshmi N. Sankar

January 2015

Performance characteristics of a transonic axial flow compressor called NASA Rotor 67 have been anal...

Effect of several porous casing treatments on stall limit and on overall performance of an axial-flow compressor rotor /

Abstract

Extracted data

Effect of several porous casing treatments on stall limit and on overall performance of an axial-flow compressor rotor /

Abstract

Extracted data

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