A streamline curvature method for design of supercritical and subcritical airfoils /

Extension of leading-edge-suction analogy to wings with separated flow around the side edges at subsonic speeds /

Lamar, John E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 24-25).Mode ...

A method for predicting shock shapes and pressure distributions on two-dimensional airfoils at large angles of attack /

Kaattari, George E.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 28.Mode of access: Internet

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : evaluation of initial perforated configuration /

Harris, Charles D., 1952-
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 14-15).Mode of access: I...

Streamline curvature design procedure for subsonic and transonic ducts /

Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

A streamline curvature method for design of supercritical and subcritical airfoils

Barger, R. L.
Brooks, C. W., Jr.

September 1974

An airfoil design procedure, applicable to both subcritical and supercritical airfoils, is described...

On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

NASA supercritical airfoils : a matrix of family-related airfoils /

Harris, Charles D., 1952-
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 14-15.Mode of access: Internet

Transonic airfoil design using cartesian coordinates /

Carlson, Leland A.
Texas A. and M. Research Foundation.
United States. National Aeronautics and Space Administration.

January 1976

Prepared by Texas A & M Research Foundation, College Station, Tex. for Langley Research Center.Cover...

A modified Theodorsen [epsilon]-function airfoil design procedure /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

A technique for generating arbitrarily shaped curved approach paths /

McConnell, Walter J.
Langley Research Center.
Sperry Flight Systems (Firm)

January 1976

"Prepared by Sperry Flight Systems ... for Langley Research Center."Cover title.Includes bibliograph...

Application of numerical optimization to the design of low-speed airfoils /

Hicks, R. M. (Raymond Morton), 1932-
Vanderplaats, Garret N.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 11).Mode of acc...

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview /

Harris, Charles D., 1952-
Brooks, Cuyler W.
Harvey, William D., 1934-
Langley Research Center.

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 22-24)...

Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight /

Badavi, F. F.
Langley Research Center.

January 1989

"Prepared for Langley Research Center under Contract NAS1-18000."Bibliography: p. 24.Mode of access:...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Extension of leading-edge-suction analogy to wings with separated flow around the side edges at subsonic speeds /

Lamar, John E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 24-25).Mode ...

A method for predicting shock shapes and pressure distributions on two-dimensional airfoils at large angles of attack /

Kaattari, George E.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 28.Mode of access: Internet

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : evaluation of initial perforated configuration /

Harris, Charles D., 1952-
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 14-15).Mode of access: I...

Streamline curvature design procedure for subsonic and transonic ducts /

Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

A streamline curvature method for design of supercritical and subcritical airfoils

Barger, R. L.
Brooks, C. W., Jr.

September 1974

An airfoil design procedure, applicable to both subcritical and supercritical airfoils, is described...

On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

NASA supercritical airfoils : a matrix of family-related airfoils /

Harris, Charles D., 1952-
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 14-15.Mode of access: Internet

Transonic airfoil design using cartesian coordinates /

Carlson, Leland A.
Texas A. and M. Research Foundation.
United States. National Aeronautics and Space Administration.

January 1976

Prepared by Texas A & M Research Foundation, College Station, Tex. for Langley Research Center.Cover...

A modified Theodorsen [epsilon]-function airfoil design procedure /

Barger, Raymond L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

A technique for generating arbitrarily shaped curved approach paths /

McConnell, Walter J.
Langley Research Center.
Sperry Flight Systems (Firm)

January 1976

"Prepared by Sperry Flight Systems ... for Langley Research Center."Cover title.Includes bibliograph...

Application of numerical optimization to the design of low-speed airfoils /

Hicks, R. M. (Raymond Morton), 1932-
Vanderplaats, Garret N.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 11).Mode of acc...

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview /

Harris, Charles D., 1952-
Brooks, Cuyler W.
Harvey, William D., 1934-
Langley Research Center.

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 22-24)...

Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight /

Badavi, F. F.
Langley Research Center.

January 1989

"Prepared for Langley Research Center under Contract NAS1-18000."Bibliography: p. 24.Mode of access:...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Extension of leading-edge-suction analogy to wings with separated flow around the side edges at subsonic speeds /

Lamar, John E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 24-25).Mode ...

A method for predicting shock shapes and pressure distributions on two-dimensional airfoils at large angles of attack /

Kaattari, George E.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 28.Mode of access: Internet

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : evaluation of initial perforated configuration /

Harris, Charles D., 1952-
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 14-15).Mode of access: I...

A streamline curvature method for design of supercritical and subcritical airfoils /

Abstract

Extracted data

A streamline curvature method for design of supercritical and subcritical airfoils /

Abstract

Extracted data

Related items

Related items