Fatigue investigation of full-scale wing panels of 7075 aluminum alloy /

Stress-corrosion cracking of aluminum alloys /

Jackson, J. D. author.
Boyd, Walter K., author.
Defense Metals Information Center (U.S.) issuing body.

Research supported by the Technology Division, Wright-Patterson Air Force Base, Ohio.Cover title."Fe...

Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds /

Arabian, Donald D.
Reid, Charles F.
Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode o...

Some recent studies in structural dynamics of rotor aircraft /

Brooks, George W.
Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

Investigation of the fatigue strength of a full-scale airplane wing structures /

Fearnow, Dwight O.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"July 13, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

Structural-loads surveys on two tilt-wing VTOL configurations /

Ward, John F.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode of ac...

Residual static strength of aluminum-alloy box beams containing fatigue cracks in the tension covers /

Leybold, Herbert A.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Stresses and loads; Structures.Includes bibliographical references.Mode of ...

Fatigue damage under varying stress amplitudes /

Liu, H. W. (Hao Wen), 1926-
Corten, H. T. (Herbert Theodore)
University of Illinois (Urbana-Champaign campus)

Prepared at the University of Illinois."November 1960."Cover title.Includes bibliographical referenc...

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

An approach to metal fatigue /

Stulen, F. B.
Schulte, W. C.
Redfern, J. H.
Curtiss-Wright Corporation.
United States. National Aeronautics and Space Administration.

January 1965

"June 1965"--- title page.Includes bibliographical references (p. 32-34).Prepared by Curtiss-Wright ...

Experimental investigation at mach number of 3.0 of the effects of thermal stress and buckling on the flutter of four-bay aluminum alloy panels with length-width ratios of 10 /

Dixon, Sidney C.
Bohon, Herman L.
Griffith, George E.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Stresses and loads; Structures.Includes bibliog...

Tensile properties and sheet-bending fatigue properties of some refractory metals at room temperature

Foster, Lee R.
Stein, Bland A.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

An analysis of the flapwise bending frequencies and mode shapes of rotor blades having two flapping hinges to reduce vibration levels /

Brooks, George W.
Leonard, H. Wayne.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Aircraft; Stresses and loads.Includes bibliographical references.Mode of...

A study of the acoustic fatigue characteristics of some flat and curved aluminum panels exposed to random and discrete noise /

Hess, R. W. (Robert W.)
Mayes, William H.
Herr, Robert W.
Langley Research Center.

January 1959

"NASA TN D-1.""Langley Research Center, Langley Field, Va.""August 1959."Cover title.Includes biblio...

Stress concentrations in filamentary structures. /

Hedgepeth, John M.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Stresses and loads; Structures.Includes bibliographical references.Mode of ac...

Stress-corrosion cracking of aluminum alloys /

Jackson, J. D. author.
Boyd, Walter K., author.
Defense Metals Information Center (U.S.) issuing body.

Research supported by the Technology Division, Wright-Patterson Air Force Base, Ohio.Cover title."Fe...

Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds /

Arabian, Donald D.
Reid, Charles F.
Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode o...

Some recent studies in structural dynamics of rotor aircraft /

Brooks, George W.
Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

Investigation of the fatigue strength of a full-scale airplane wing structures /

Fearnow, Dwight O.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"July 13, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

Structural-loads surveys on two tilt-wing VTOL configurations /

Ward, John F.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode of ac...

Residual static strength of aluminum-alloy box beams containing fatigue cracks in the tension covers /

Leybold, Herbert A.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Stresses and loads; Structures.Includes bibliographical references.Mode of ...

Fatigue damage under varying stress amplitudes /

Liu, H. W. (Hao Wen), 1926-
Corten, H. T. (Herbert Theodore)
University of Illinois (Urbana-Champaign campus)

Prepared at the University of Illinois."November 1960."Cover title.Includes bibliographical referenc...

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

An approach to metal fatigue /

Stulen, F. B.
Schulte, W. C.
Redfern, J. H.
Curtiss-Wright Corporation.
United States. National Aeronautics and Space Administration.

January 1965

"June 1965"--- title page.Includes bibliographical references (p. 32-34).Prepared by Curtiss-Wright ...

Experimental investigation at mach number of 3.0 of the effects of thermal stress and buckling on the flutter of four-bay aluminum alloy panels with length-width ratios of 10 /

Dixon, Sidney C.
Bohon, Herman L.
Griffith, George E.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Stresses and loads; Structures.Includes bibliog...

Tensile properties and sheet-bending fatigue properties of some refractory metals at room temperature

Foster, Lee R.
Stein, Bland A.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

An analysis of the flapwise bending frequencies and mode shapes of rotor blades having two flapping hinges to reduce vibration levels /

Brooks, George W.
Leonard, H. Wayne.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Aircraft; Stresses and loads.Includes bibliographical references.Mode of...

A study of the acoustic fatigue characteristics of some flat and curved aluminum panels exposed to random and discrete noise /

Hess, R. W. (Robert W.)
Mayes, William H.
Herr, Robert W.
Langley Research Center.

January 1959

"NASA TN D-1.""Langley Research Center, Langley Field, Va.""August 1959."Cover title.Includes biblio...

Stress concentrations in filamentary structures. /

Hedgepeth, John M.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Stresses and loads; Structures.Includes bibliographical references.Mode of ac...

Stress-corrosion cracking of aluminum alloys /

Jackson, J. D. author.
Boyd, Walter K., author.
Defense Metals Information Center (U.S.) issuing body.

Research supported by the Technology Division, Wright-Patterson Air Force Base, Ohio.Cover title."Fe...

Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds /

Arabian, Donald D.
Reid, Charles F.
Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode o...

Some recent studies in structural dynamics of rotor aircraft /

Brooks, George W.
Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Fatigue investigation of full-scale wing panels of 7075 aluminum alloy /

Abstract

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Fatigue investigation of full-scale wing panels of 7075 aluminum alloy /

Abstract

Extracted data

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