Browse TRAIL Inventories

Effect of variation in rivet strength on the average stress at maximum load for aluminum-alloy, flat, z-stiffened compression panels that fail by local buckling

Effect of type of porous surface and suction velocity distribution on the characteristics of a 10.5-percent-thick airfoil with area suction

Experiments on mixed-free-and-forced-convective heat transfer connected with turbulent flow through a short tube

Effect of prestraining of recrystallization temperature and mechanical properties of commercial, sintered, wrought molybdenum

Evaluation of gust response characteristics of some existing aircraft with wing bending flexibility included

Effects of symmetric and asymmetric thrust reversal on the aerodynamic characteristics of a model of a twin-engine airplane

Estimated power reduction by water injection in a nonreturn supersonic wind tunnel

An experimental investigation of secondary flow in an accelerating, rectangular elbow with 90 degrees of turning

Experimental investigation of the effects of cooling on friction and on boundary-layer transition for low-speed gas flow at the entry of a tube

Experimental investigation of the effect of rear-fuselage shape on ditching behavior

Surveys of the flow fields at the propeller planes of six 40 degree sweptback wing-fuselage-nacelle combinations

Summary of revised gust-velocity data obtained from V-G records taken on civil transport airplanes from 1933 to 1950

Propeller-performance charts for transport airplanes

Study of pressure effects on vaporization rate of drops in gas streams

Studies of the use of Freon-12 as a wind tunnel testing medium

Survey of portions of the iron-nickel-molybdenum and cobalt-iron-molybdenum ternary systems at 1200 C

Experimental stress analysis of stiffened cylinders with cutouts: Pure torsion

The Sodium Hydroxide Reactor - Effect of Reactor Variables on Criticality and Fuel- Element Temperature Requirements for Subsonic and Supersonic Aircraft Nuclear Propulsion

Preliminary Results of Heat Transfer from a Stationary and Rotating Ellipsoidal Spinner

Stability and Control Characteristics at High Subsonic Speeds of a 1/30-Scale Model of the MX-1554A Design

Stability and Control Characteristics at Low Speed of a Modified 1/10-Scale Model of the MX-1554A Design

Stability and Control Characteristics at Low Speed of a 1/10-Scale Model of MX-1554A Design

An Investigation of the Dynamic and Static Stability Characteristics of a Group of Specialized Store Configurations at Transonic Speeds

Transonic Aerodynamic and Trim Characteristics of 1/15-Scale Models of the Convair MX-1964 Airplane With Indented Fuselage

Results of a Power-on Flight of a 1/10-Scale Rocket-Propelled Model of the Convair XF2Y-1 Airplane at a Mach Number of 1.53

Wind-Tunnel Investigation of a 1/60-Scale Model of the Republic MX-1554 Airplane at a Mach Number of 2.85

Wind-Tunnel Investigation of the Drag and Lateral-Stability Characteristics of a 1/22-Scale Model of a Bomber Airplane Employing a Low-Aspect-Ratio Triangular Wing

Theoretical Performance of Liquid Hydrogen and Liquid Fluorine as a Rocket Propellant

Theoretical Performance of Mixtures of Liquid Ammonia and Hydrazine as Fuel With Liquid Fluorine as Oxidant for Rocket Engines

Theoretical Performance of Liquid Hydrazine and Liquid Fluorine as a Rocket Propellant

Theoretical Performance of Liquid Ammonia and Liquid Fluorine as a Rocket Propellant

An Investigation Utilizing an Electrical Analogue of Cyclic Deicing of Hollow Steel Propellers with Internal Electric Heaters

Impingement of Water Droplets on NACA 65(1)-208 and 65(1)-212 Airfoils at 4 Degrees Angle of Attack

Maximum Evaporation Rates of Water Droplets Approaching Obstacles in the Atmosphere Under Icing Conditions

The Effects of Extensible Rocket Racks on Lift, Drag, and Stability of a 1/10 Scale Rocket-Boosted Model of the McDonnell XF3H-1 Airplane for a Mach Number Range of 0.60 to 1.34

Development of a Supersonic Area Rule and an Application to the Design of a Wing-Body Combination Having High Lift-to-Drag Ratios

Drag and Static Stability at Low Lift of Rocket-Powered Models of the Convair MX-1626 Airplane at Mach Numbers From 0.7 to 1.5

Effect of Ice and Frost Formations on Drag of NACA 65(sub 1) -212 Airfoil for Various Modes of Thermal Ice Protection

Nonuniform Burnup and Poisoning Effects in a Reactor and Validity of Uniform Approximation

Rocket Engine Starting With Mixed Oxides of Nitrogen and Liquid Ammonia by Flow-Line Additives

Effect of Fuel Injectors and Liner Design on Performance of an Annular Turbojet Combustor With Vapor Fuel

Examination of Recent Lateral-Stability-Derivative Data

An Analysis of a Nuclear Powered Supercritical-Water Cycle for Aircraft Propulsion

Altitude Performance of a 20-Inch-Diameter Ram-Jet Engine Investigated in a Free-Jet Facility at Mach Number 3.0

Analytical Investigation of Icing Limit for Diamond-Shaped Airfoil in Transonic and Supersonic Flow

A Method for Calculating the Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic, Transonic, and Supersonic Speeds

A Method for Rapid Determination of the Icing Limit of a Body in Terms of the Stream Conditions

Investigation of Aerodynamic and Icing Characteristics of a Flush Alternate Inlet Induction System Air Scoop

Analytical Studies of the Response to Longitudinal Control of Three Airplane Configurations in Landing Approaches

Aerodynamic Characteristics of Low-aspect-ratio Wings at High Supersonic Mach Numbers


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