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Turbulent Convective Heat-Transfer Coefficients Measured From Flight Tests of Four Research Models (NACA RM-10) at Mach Numbers From 1.0 to 3.6 (open access)

Turbulent Convective Heat-Transfer Coefficients Measured From Flight Tests of Four Research Models (NACA RM-10) at Mach Numbers From 1.0 to 3.6

Report presenting an evaluation of convective heat-transfer coefficients from skin temperatures measured along the body of a research model designated NACA RM-10. Heat-transfer data is presented for a range of Mach and Reynolds numbers based on the axial distance from the nose to the point at which the temperature measurements were made. Results regarding the recovery factor, heat transfer, correlation with different aircraft models, and Reynolds analogy are provided.
Date: March 11, 1955
Creator: Chauvin, Leo T. & Maloney, Joseph P.
System: The UNT Digital Library
[Herman Lurie's Weekly Report, March 11, 1955] (open access)

[Herman Lurie's Weekly Report, March 11, 1955]

Herman Lurie's weekly report for the sugar market.
Date: March 11, 1955
Creator: Lurie, Herman
System: The Portal to Texas History
A COMPARISON BETWEEN BARE AND BLACKENED PORCINE SKIN IN RESPONSE TO PULSES OF HIGH INTENSITY RADIANT THERMAL ENERGY (open access)

A COMPARISON BETWEEN BARE AND BLACKENED PORCINE SKIN IN RESPONSE TO PULSES OF HIGH INTENSITY RADIANT THERMAL ENERGY

None
Date: March 11, 1955
Creator: Mixter, G. Jr.
System: The UNT Digital Library
The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselagestore Configurations 1. - Swept-Wing Heavy-Bomber Configuration With Large Store (Nacelle). Lift and Drag; Mach Number, 1.61 (open access)

The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselagestore Configurations 1. - Swept-Wing Heavy-Bomber Configuration With Large Store (Nacelle). Lift and Drag; Mach Number, 1.61

Memorandum presenting a supersonic wind-tunnel investigation of the origin and distribution of store interference in the 4- by 4-foot supersonic pressure tunnel at Mach number 1.6 in which separate forces on a store, a fuselage, a swept wing, and a swept-wing-fuselage combination were measured. The store was separately sting-mounted on its own six-component internal balance and was traversed through a wide systematic range of spanwise, chordwise, and vertical positions.
Date: March 11, 1955
Creator: Smith, Norman F. & Carlson, Harry W.
System: The UNT Digital Library
Flight Measurements of the Transonic Drag of Models of Several Isolated External Stores and Nacelles (open access)

Flight Measurements of the Transonic Drag of Models of Several Isolated External Stores and Nacelles

Report presenting drag measurements on models of 20 isolated external stores and nacelles flown from the helium gun at a range of Mach numbers. Results regarding fineness-ratio and shape effects, drag correlation, and friction drag are provided. Generally, the shape variations among the various types of stores and nacelles had the expected effects on isolated body drag.
Date: March 11, 1955
Creator: Stevens, Joseph E. & Purser, Paul E.
System: The UNT Digital Library
[Texas Imperial Company Form 1120, U. S. Corporation Income Tax Return: 1954] (open access)

[Texas Imperial Company Form 1120, U. S. Corporation Income Tax Return: 1954]

Corporate income tax return of 1954 for Texas Imperial Company. The return includes all necessary schedules. The Schedule PH, Computation of Personal Holding Company Tax, is also included.
Date: March 11, 1955
Creator: Texas Imperial Company
System: The Portal to Texas History