Edward C. Polhamus

发表

RESEARCH MEMORANDUM AERODYNAMIC CIylRACTEmTICS WITH FEED AND FRcEE TRAN;SITION OF A MODIFIED DELTA WINGIN COMBINATION WITH A FUSEIAGE AT EIGE SUBSONIC SPEEDS

Edward C. Polhamus, 1950 .

High-Speed Wind-Tunnel Investigation of the Longitudinal Stability and Control Characteristics of a 0.10-Scale Model of the Grumman XF9F-2 Airplane, TED No. NACA DE301

Edward C. Polhamus, Thomas J. King, 1948 .

A Simple Method of Estimating the Subsonic Lift and Damping in Roll of Sweptback Wings

Edward C. Polhamus, 1949 .

THE EFFECTS OF HORIZONTAL-TAIL POSITION ON THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT TRANSONIC SPEEDS OF A VARIABLE-SWEEP AIRCRAFT HAVING AN INBOARD PIVOT

Edward C. Polhamus, Alexander D. Hammond, 1961 .

Wind-Tunnel Investigation of Bomb-Bay Configurations Intended to Minimize the Tumbling of Light-Weight Bombs

Richard E. Kuhn, Edward C. Polhamus, 1947 .

High-Speed Wind-Tunnel Investigation of the Lateral Stability Characteristics of a 0.10-Scale Model of the Grumman XF9F-2 Airplane, TED No. NACA DE 301

Edward C. Polhamus, Thomas J. King, 1949 .

EXPERIMENTAL AND THEORETICAL STUDIES OF THE EFFECTS OF CAMBER AND TWIST ON THE AERODYNAMIC CHARACTERISTICS OF PARAWINGS HAVING NOMINAL ASPECT RATIOS OF 3 AND 6

Edward C. Polhamus, R. L. Naeseth, Rodger L. Naeseth, 1963 .

Application of slender wing benefits to military aircraft

Edward C. Polhamus, E. Polhamus, 1983 .

Aerodynamic characteristics with fixed and free transition of a modified delta wing in combination with fuselage at high subsonic speeds

Edward C. Polhamus, Thomas J. King, E. Polhamus, 1950 .

Technical evaluation report on the fluid dynamics panel symposium on high angle of attack aerodynamics

Edward C. Polhamus, 1979 .

Wind-Tunnel Investigation of the Stability and Control Characteristics of a Complete Model Equipped With a Vee Tail

Edward C. Polhamus, Robert J. Moss, 1947 .

Pressure and Force Characteristics of Noncircular Cylinders as Affected by Reynolds Number with a Method Included for Determining the Potential Flow About Arbitrary Shapes

Edward C. Polhamus, Edward W. Geller, Kalman J. Grunwald, 1959 .

Aerodynamic Characteristics of Tapered Wings Having Aspect Ratios of 4, 6, and 8, Quarter-chord Lines Swept Back 45 Degrees, and NACA 63(sub 1)A012 Airfoil Sections : Transonic-bump Method

Edward C. Polhamus, Thomas J. King, 1951 .