Comparison of two- and three-dimensional flow computations with laser anemometer measurements in a transonic compressor rotor /

Three component laser anemometer measurements in an annular cascade of core turbine vanes with contoured end wall /

Goldman, Louis J.
Seasholtz, Richard G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"November 1988"--Cover.Includes bibliographical references (p. 14).Mode of access: Internet

Calculation of three-dimensional unsteady transonic flows past helicopter blades /

Chattot, J. J.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Aeromechanics Laboratory"--Cover.Includes bibliographical references.Mode of access: Inte...

Improved method for calculating transonic velocities on blade-to-blade stream surfaces of a turbomachine /

Wood, Jerry R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1981

STAR category 02."April 1981"--Cover."Lewis Research Center."Includes bibliographical references.Mod...

Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies /

Reyhner, Theodore A.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Transonic flow analysis for rotors.

Chang, I-Chung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1990

"June 1990."Cover title.Distributed to depository libraries in microfiche.Includes bibliographical r...

Laser anemometer measurements in an annular cascade of core turbine vanes and comparison with theory /

Goldman, Louis J.
Seasholtz, Richard G.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"June 1982"--Cover.STAR category 02."Lewis Research Center."Includes bibliographical references.Mode...

Experimental investigation of a transonic compressor cascade and test results for four blade sections /

Emery, James C.
Westphal, Willard R.
Dunavant, James C.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bliographical references (p. 10).Mode of access: Internet

High-speed laser anemometer system for intrarotor flow mapping in turbomachinery /

Powell, J. Anthony.
Seasholtz, Richard G.
Strazisar, Anthony J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1982

"Lewis Research Center.""February 1982"--Cover.Includes bibliographical references.Mode of access: I...

Transonic pressure measurements and comparison of theory to experiment for three arrow-wing configurations : summary report /

Manro, Marjorie E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."February 1982"--Cover.Includes bibliographical references.Mode of access: Inter...

Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row /

Farrell, Charles A.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 02."June 1982"--Cover."Lewis Research Center."Includes bibliographical references.Mode...

Performance comparisons of high mach number compressor rotor blading /

Gostelow, J. P.
Smith, L. H.
Krabacher, K. W.
Lewis Research Center.
General Electric Company.
United States. National Aeronautics and Space Administration.

January 1968

"December 1968."Includes bibliographical references."Prepared under contract no.Mode of access: Inte...

Two-dimensional analytical and experimental performance comparison for a compressor stator section with d-factor of 0.47 /

Sanger, Nelson L.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 27-28).Mode of...

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

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Lewis, George W., Jr.
Serovy, G. K. (George K.)
Schwenk, Francis C.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"Declassified October 31, 1958.""April 5, 1954."Cover title.Includes bibliographical references (p. ...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Three component laser anemometer measurements in an annular cascade of core turbine vanes with contoured end wall /

Goldman, Louis J.
Seasholtz, Richard G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"November 1988"--Cover.Includes bibliographical references (p. 14).Mode of access: Internet

Calculation of three-dimensional unsteady transonic flows past helicopter blades /

Chattot, J. J.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Aeromechanics Laboratory"--Cover.Includes bibliographical references.Mode of access: Inte...

Improved method for calculating transonic velocities on blade-to-blade stream surfaces of a turbomachine /

Wood, Jerry R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1981

STAR category 02."April 1981"--Cover."Lewis Research Center."Includes bibliographical references.Mod...

Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies /

Reyhner, Theodore A.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Transonic flow analysis for rotors.

Chang, I-Chung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1990

"June 1990."Cover title.Distributed to depository libraries in microfiche.Includes bibliographical r...

Laser anemometer measurements in an annular cascade of core turbine vanes and comparison with theory /

Goldman, Louis J.
Seasholtz, Richard G.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"June 1982"--Cover.STAR category 02."Lewis Research Center."Includes bibliographical references.Mode...

Experimental investigation of a transonic compressor cascade and test results for four blade sections /

Emery, James C.
Westphal, Willard R.
Dunavant, James C.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bliographical references (p. 10).Mode of access: Internet

High-speed laser anemometer system for intrarotor flow mapping in turbomachinery /

Powell, J. Anthony.
Seasholtz, Richard G.
Strazisar, Anthony J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1982

"Lewis Research Center.""February 1982"--Cover.Includes bibliographical references.Mode of access: I...

Transonic pressure measurements and comparison of theory to experiment for three arrow-wing configurations : summary report /

Manro, Marjorie E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."February 1982"--Cover.Includes bibliographical references.Mode of access: Inter...

Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row /

Farrell, Charles A.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 02."June 1982"--Cover."Lewis Research Center."Includes bibliographical references.Mode...

Performance comparisons of high mach number compressor rotor blading /

Gostelow, J. P.
Smith, L. H.
Krabacher, K. W.
Lewis Research Center.
General Electric Company.
United States. National Aeronautics and Space Administration.

January 1968

"December 1968."Includes bibliographical references."Prepared under contract no.Mode of access: Inte...

Two-dimensional analytical and experimental performance comparison for a compressor stator section with d-factor of 0.47 /

Sanger, Nelson L.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 27-28).Mode of...

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

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Lewis, George W., Jr.
Serovy, G. K. (George K.)
Schwenk, Francis C.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"Declassified October 31, 1958.""April 5, 1954."Cover title.Includes bibliographical references (p. ...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Three component laser anemometer measurements in an annular cascade of core turbine vanes with contoured end wall /

Goldman, Louis J.
Seasholtz, Richard G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"November 1988"--Cover.Includes bibliographical references (p. 14).Mode of access: Internet

Calculation of three-dimensional unsteady transonic flows past helicopter blades /

Chattot, J. J.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Aeromechanics Laboratory"--Cover.Includes bibliographical references.Mode of access: Inte...

Improved method for calculating transonic velocities on blade-to-blade stream surfaces of a turbomachine /

Wood, Jerry R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1981

STAR category 02."April 1981"--Cover."Lewis Research Center."Includes bibliographical references.Mod...

Comparison of two- and three-dimensional flow computations with laser anemometer measurements in a transonic compressor rotor /

Abstract

Extracted data

Comparison of two- and three-dimensional flow computations with laser anemometer measurements in a transonic compressor rotor /

Abstract

Extracted data

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