Correlation of part-span damper losses through transonic rotors operating near design point /

Exploratory investigation of the moments on oscillating control surfaces at transonic speeds /

Martin, Dennis J.
Martz, C. William.
Thompson, Robert F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"August 15, 1955."Includes bibliographical references (p. 9-10).Mode of access: Internet

Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stage /

Moore, Royce D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."September 1982."Includes bibliographical references.Mode of access: Internet

Transonic flutter tests of a highly swept arrow wing with and without simulated trailing-edge-mounted engine masses /

Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inte...

Critical-speed analysis of flexibly mounted rigid rotors /

Cavicchi, Richard H.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 50).Mode of access: Internet

Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft /

Mineck, Raymond E.
United States. National Aeronautics and Space Administration.

January 1977

Issued Sept. 1977.Includes bibliographical references (p. 14).Mode of access: Internet

Correlation of part-span damper losses through transonic rotors operating near design point

Roberts, W. B.

June 1977

The design-point losses caused by part-span dampers (PSD) were correlated for 21 transonic axial flo...

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...

Effect of a reduction in stator solidity on performance of a transonic turbine /

Miser, James W.
Wong, Robert Y.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified December 3, 1958.""March 23, 1956."Cover title.Includes bibliographical references (p....

Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model /

Althoff, Susan L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"September 1988"--Cover.Includes bibliographical references (p. 7-8).Mode of access: Internet

An experimental investigation of the effects of Mach number, stabilizer dihedral, and fin torsional stiffness on the transonic flutter characteristics of a tee-tail /

Land, Norman S.
Fox, Annie G.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"October 23, 1957."Includes bibliographical references (p. 8).Mode of access: Internet

Flutter characteristics of swept wings at transonic speeds /

Loftin, Laurence K.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"July 6, 1955."Includes bibliographical references (p. 10).Mode of access: Internet

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...

Review of propeller-rotor whirl flutter /

Reed, Wilmer H., III.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Work performed at Langley Research Center."July 1967."Includes bibliographical references (p. 26-27)...

Transient dynamics of a flexible rotor with squeeze film dampers /

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Buono, D. F.
United Technologies Corporation.

January 1978

Sept. 1978.Contract NAS3-18523.Includes bibliographical references.Mode of access: Internet

Hydrodynamic damping and "added mass" for flexible offshore platforms /

Petrauskas, Charles
Coastal Engineering Research Center (U.S.)

"October 1976."Includes bibliographical references (pages 102-105).Mode of access: Internet

Exploratory investigation of the moments on oscillating control surfaces at transonic speeds /

Martin, Dennis J.
Martz, C. William.
Thompson, Robert F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"August 15, 1955."Includes bibliographical references (p. 9-10).Mode of access: Internet

Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stage /

Moore, Royce D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."September 1982."Includes bibliographical references.Mode of access: Internet

Transonic flutter tests of a highly swept arrow wing with and without simulated trailing-edge-mounted engine masses /

Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inte...

Critical-speed analysis of flexibly mounted rigid rotors /

Cavicchi, Richard H.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 50).Mode of access: Internet

Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft /

Mineck, Raymond E.
United States. National Aeronautics and Space Administration.

January 1977

Issued Sept. 1977.Includes bibliographical references (p. 14).Mode of access: Internet

Correlation of part-span damper losses through transonic rotors operating near design point

Roberts, W. B.

June 1977

The design-point losses caused by part-span dampers (PSD) were correlated for 21 transonic axial flo...

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...

Effect of a reduction in stator solidity on performance of a transonic turbine /

Miser, James W.
Wong, Robert Y.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified December 3, 1958.""March 23, 1956."Cover title.Includes bibliographical references (p....

Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model /

Althoff, Susan L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"September 1988"--Cover.Includes bibliographical references (p. 7-8).Mode of access: Internet

An experimental investigation of the effects of Mach number, stabilizer dihedral, and fin torsional stiffness on the transonic flutter characteristics of a tee-tail /

Land, Norman S.
Fox, Annie G.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"October 23, 1957."Includes bibliographical references (p. 8).Mode of access: Internet

Flutter characteristics of swept wings at transonic speeds /

Loftin, Laurence K.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"July 6, 1955."Includes bibliographical references (p. 10).Mode of access: Internet

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...

Review of propeller-rotor whirl flutter /

Reed, Wilmer H., III.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Work performed at Langley Research Center."July 1967."Includes bibliographical references (p. 26-27)...

Transient dynamics of a flexible rotor with squeeze film dampers /

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Buono, D. F.
United Technologies Corporation.

January 1978

Sept. 1978.Contract NAS3-18523.Includes bibliographical references.Mode of access: Internet

Hydrodynamic damping and "added mass" for flexible offshore platforms /

Petrauskas, Charles
Coastal Engineering Research Center (U.S.)

"October 1976."Includes bibliographical references (pages 102-105).Mode of access: Internet

Exploratory investigation of the moments on oscillating control surfaces at transonic speeds /

Martin, Dennis J.
Martz, C. William.
Thompson, Robert F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"August 15, 1955."Includes bibliographical references (p. 9-10).Mode of access: Internet

Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stage /

Moore, Royce D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."September 1982."Includes bibliographical references.Mode of access: Internet

Transonic flutter tests of a highly swept arrow wing with and without simulated trailing-edge-mounted engine masses /

Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inte...

Correlation of part-span damper losses through transonic rotors operating near design point /

Abstract

Extracted data

Correlation of part-span damper losses through transonic rotors operating near design point /

Abstract

Extracted data

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