Scientism and Values. Edited by Helmut Schoeck and James W. Wiggins
Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45° Sweptback Wing at High Subsonic Speeds
A Genealogical History of the Descendants of Peter White, of New Jersey, from 1670
Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13° and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives
Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives
Reports of Cases Argued and Determined in the Supreme Court of the State of Kansas. Published Under Authority of Law by Direction of the Supreme Court of Kansas
Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds
Civil Procedure Reports
Psychiatry and Responsibility. Edited by H. Schoeck and James W. Wiggins. Papers by Thomas S. Szasz [and Others], Etc
Relativism and the Study of Man; Papers by Leonard Carmichael And Others Edited by Helmut Schoeck and James W. Wiggins
The New Argument in Economics. The Public Versus the Private Sector. [By Various Authors.] Edited by Helmut Schoeck and James W. Wiggins, Etc
Foreign Aid Reexamined
The New Argument in Economics. The Public Versus the Private Sector. D. by Helmut Schoeck, James W. Wiggins
Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45° Sweptback Wing at High Subsonic Speeds
Central Planning and Neomercantilism, Edited by Helmut Schoeck and James W. Wiggins. Papers by Garrett Hardin [and Others].
Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13° and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives
Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds
Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives
Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch of Wing-fuselage Combinations at High Subsonic Speeds
Central Planning and Neomercantilism