Ira H. Abbott

Ira H. Abbott, at the right.

Ira H. Abbott (July 18, 1906 – November 3, 1988) was an American aerospace engineer. A graduate of MIT, Abbott worked for Langley Aeronautical Laboratory in 1929. He was a Director of Aeronautical and Space Research at NASA during the middle of the twentieth century and before that was employed by the National Advisory Committee for Aeronautics (NACA). Abbott supervised the X-15, supersonic transport, nuclear rocket and advanced reentry programs. He retired in 1962.^[1] As Assistant Director of NACA, Abbott was decisive in keeping Ames Research Center focused on research instead of moving into operations during the development of the proposed Orbiting Astronomical Observatory in the 1960.^[2]

Bibliography

• Abbott co-authored the reference book Theory of Wing Sections, including a summary of airfoil data, with Albert E. von Doenhoff in 1949.^[3]

References

• "Test if a Highly Cambered Low-Drag-Airfoil Section with a Lift Control Flap, Special Report", 1942, NASA Technical Report Server.

• "Preliminary Investigation of Certain Laminar-Flow Airfoils for Application at High Speeds and Reynolds Numbers", 1939, NASA Technical Report Server.

• ".Summary of Airfoil Data ",1945, NASA Technical Report Server

• "Pressure-Distribution Measurements of a Model of a Davis Wing Section with Fowler Flap Submitted by Consolidated Aircraft Corporation",1942, NASA Technical Report Server.

• "The NACA variable-density wind tunnel",1933,NASA Technical Report Server.

• "The design of low-turbulence wind tunnels",1949,NASA Technical Report Server.

• "Fuselage-drag tests in the variable-density wind tunnel: streamline bodies of revolution, fineness ratio of 5",1937, NASA Technical Report Server.

• "Title: Pressure-distribution measurements of two airfoil models with Fowler flaps submitted by Consolidated Aircraft Corporation as alternative wing sections of the XB-32 airplane",1942,NASA Technical Report Server.

• "Tests in the variable-density wind tunnel of the NACA 23012 airfoil with plain and split flaps",1939,NASA Technical Report Server.

• "Experiments with a model water tunnel",1930, NASA Technical Report Server.

• "Aerodynamic characteristics of NACA 23012 and 23021 airfoils with 20-percent-chord external-airfoil flaps of NACA 23012 section",1937,NASA Technical Report Server.

• "Airship model tests in the variable density wind tunnel",1932,NASA Technical Report Server.

• "Airfoil section data obtained in the NACA variable-density tunnel as affected by support interference and other corrections",1939,NASA Technical Report Server.

• "The design of low-turbulence wind tunnels",1949, NASA Technical Report Server.

• " The drag of two streamline bodies as affected by protuberances and appendages",1934,NASA Technical Report Server.

• " Tests of four models representing intermediate sections of the XB-33 airplane including sections with slotted flap and ailerons",1942, NASA Technical Report Server.

• "Interference effects of longitudinal flat plates on low-drag airfoils",1942,NASA Technical Report Server.

• "Flow observations with tufts and lampblack of the stalling of four typical airfoil sections in the NACA variable-density tunnel",1938, NASA Technical Report Server.

• Launius, Roger D.. "History Home". NASA History Office Home Page. Retrieved January 26, 2010.