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Technical Report Archive and Image Library
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Bibliography : Impact Testing of Materials
Reactivity of the Critical Experiment as a Function of Gap Width
Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) 2: aerodynamic load distributions of series of five bodies having conical noses and cylindrical afterbodies
Development of Metal-Bonding Adhesive FPL-710 With Improved Heat-Resistant Properties
Forces and moments on pointed blunt-nosed bodies of revolution at Mach numbers from 2.75 to 5.00
Effects of internal configuration on afterburner shell temperatures
An analytical method for evaluating factors affecting application of transpiration cooling to gas turbine blades
Longitudinal Stability and Control Characteristics of a Canard Missile Configuration for Mach Numbers From 1.1 to 1.93 as Determined From Free-Flight and Wind-Tunnel Investigation
The transonic characteristics of 38 cambered rectangular wings of varying aspect ratio and thickness as determined by the transonic-bump technique
Lateral-control investigation at transonic speeds of retractable spoiler and plug-type spoiler-slot ailerons on a tapered 60 degree sweptback wing of aspect ratio 2 : transonic-bump method
Transonic Drag Characteristics and Pressure Distribution on the Body of a Wing-Body Combination Consisting of a Body of Revolution of Fineness Ratio 12 and a Wing Having Sweepback of 45 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Sections
An experimental cascade study of the effects of a solidity reduction on the two-dimensional aerodynamic characteristics of a turbine-rotor blade suitable for air cooling
Preliminary investigation at transonic speeds of the effect of balancing tabs on the hinge-moment and other aerodynamic characteristics of a full-span flap on a tapered 45 degree sweptback wing of aspect ratio 3
Altitude operational characteristics of a prototype model of the J47D (RX1-1 and RX1-3) turbojet engines with integrated electronic control
Investigation of effects of additives on storage properties of fuming nitric acids
Effect of Aspect Ratio on the Low-Speed Lateral Control Characteristics of Untapered Low-Aspect-Ratio Wings Equipped With Flap and With Retractable Ailerons
Air Sampling Chamber for S.I.R.
Preliminary Investigation of Monochromatic X-ray Absorption as a Method of Analysis for Uranium
Preliminary Data on the Phase Equilibrium Systems UO₂ - MgO ; U³O⁸ - MgO ; UO₂ - Nd²O³ ; U³O⁸ - Nd²O³ ; and UO₂ - Al²O³
The [beta]-Spectra of Pu²³⁹, Pu²⁴⁰, Pu²⁴¹and Sm¹⁵¹
Mathematics Panel Quarterly Progress Report for the Period Ending October 31,1951
Summary of the Research Progress Meetings for January, 1952.
MTA Mark II Accelerator, Drift Tube and RF Beam Geometry Perturbing Effect of Beam in A-12
Comparison between prediction and experiment for all-movable wing and body combinations at supersonic speeds: Lift, pitching moment, and hinge moment
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