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Some Wind-Tunnel Experiments on Single-Degree-of-Freedom Flutter of Ailerons in the High Subsonic Speed Range

Preliminary Report on Experimental Investigation of Engine Dynamics and Controls for a 48-Inch Ram-Jet Engine

Preliminary Measurements of the Aerodynamic Yawing Derivatives of a Triangular, a Swept, and an Unswept Wing Performing Pure Yawing Oscillations, With a Description of the Instrumentation Employed

Tabulation of Mass-Flow Parameters for Use in Design of Turbomachine Blade Rows for Ratios of Specific Heats of 1.3 and 1.4

Comparison of the Minimum Drag of Two Versions of a Modified Delta-Wing Fighter as Obtained From Flight Tests of Rocket-Boosted Models and Equivalent Bodies Between Mach Numbers of 0.80 and 1.64

Turbojet Performance and Operation at High Altitudes With Hydrogen and JP-4 Fuels

Turbulent and Laminar Heat-Transfer Measurements on a 1/6-Scale NACA RM-10 Missile in Free Fight to Mach Number of 4.2 and to a Wall Temperature of 1400 Degrees R

Transonic Aerodynamic Characteristics of a 1/15-Scale Model of the Convair B-58 Airplane

Turbulent-Heat-Transfer Measurements at a Mach Number of 3.90

The Use of Area Suction for Improving the Longitudinal Characteristics of a Thin Unswept Wing-Fuselage Model With Leading- and Trailing-Edge Flaps

Two Experiments on Applications of the Transonic Area Rule to Asymmetric Configurations

Results of Rocket Model Test of an Airplane Configuration Having an Arrow Wing and Slender Flat-Sided Fuselage: Lift, Drag, Longitudinal Stability, Lateral Force, and Jet Effects at Mach Numbers Between 1.0 and 2.3

Static Shear Strength of 2117-T4 (A17S-T4) Aluminum-Alloy Rivets at Elevated Temperatures

The Subsonic Lateral and Longitudinal Static Stability Characteristics Up to Large Angles of Sideslip for a Triangular-Wing Airplane Model Having a Ventral Fin

Supersonic Investigation of the Lift, Drag, Static Stability, and Hinge-Moment Characteristics of a Rocket-Powered Model of a Ballistic-Missile Configuration

A Semiempirical Procedure for Estimating Wing Buffet Loads in the Transonic Region

A Semigraphical Method for the Determination of the Rolling Characteristics of Rolleron-Equipped Missiles

Pressure Distributions on Four Canopy-Fuselage Configurations at Transonic Speeds

Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6

Some Effects of Sweep and Thickness on the Experimental Downwash Characteristics at Transonic Speeds of a Series of Highly Tapered Wings With an Aspect Ratio of 3: Transonic Bump Method

Some Notes on the Violent Lateral-Longitudinal Coupling Motions of the Douglas X-3 Airplane in Aileron Rolls

The Static and Dynamic-Rotary Stability Derivatives at Subsonic Speeds of an Airplane Model With an Unswept Wing and a High Horizontal Tail

A Transonic Wind-Tunnel Investigation of Store and Horizontal-Tail Loads and Some Effects of Fuselage-Afterbody Modifications on a Swept-Wing Fighter Airplane

Use of Shadowgraph Technique in the Analysis of the Performance of Two Supersonic Axial-Flow Compressor Rotors Operating Over a Mean Radius Relative Inlet Mach Number Range of 0.85 to 1.7

Wind-Tunnel Investigation of a Ram-Jet Model Having a Wing and Canard Surfaces of Delta Plan Form With 70 Degrees Swept Leading Edges: Force and Moment Characteristics at Combined Angles of Pitch and Sideslip for Mach Number 2.01

Wind-Tunnel Investigation at High Subsonic Speeds of Some Effects of Fuselage Cross-Section Shape and Wing Height on the Static Longitudinal and Lateral Stability Characteristics of a Model Having a 45 Degree Swept Wing

The Variation With Wing Aspect Ratio of Flap Effectiveness on Thin Rectangular Wings at Transonic Speeds

Wind-Tunnel Investigation at Low Speed of Effects of Sideslip on Static Longitudinal Trim and Static Lateral Stability Characteristics of Three Fighter-Type Airplane Models

Wind-Tunnel Investigation at Mach Numbers From 0.8 to 1.4 of Static Longitudinal and Lateral-Directional Characteristics of an Unswept-Wing Airplane Model

Wind-Tunnel Investigation at Transonic Speeds of a Jet Control on a 35 Degree Swept Wing: Transonic-Bump Method

A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback-Wing-Body Combination Designed for High Performance

Transonic Investigation of the Effectiveness and Loading Characteristics of a Flap-Type Aileron With and Without Paddle Balances of an Unswept-Wing-Fuselage Model

Transonic Wind-Tunnel Investigation of Static Longitudinal Force and Moment Characteristics of Two Wing-Body Combinations With Clipped-Tip and Full Delta Wings of Aspect Ratio 1.73

A Transonic Investigation of the Static Longitudinal-Stability Characteristics of a 45 Degree Sweptback Wing-Fuselage Combination With and Without Horizontal Tail

Transonic Wind-Tunnel Investigation of the Effects of a Heated Propulsive Jet on the Pressure Distribution Along a Fuselage Overhang

Experimental and Theoretical Studies of Interference Effects on the Damping in Roll of the Bell X-1A Research Airplane at Supersonic Speeds (Including Canopy Shape Effects)

A Method of Reducing Heat Transfer to Blunt Bodies by Air Injection

Wing-Body Combinations With Wings of Very Low Aspect Ratio at Supersonic Speeds

The Effects of Compressibility on the Upwash at the Propeller Planes of a Four-Engine Tractor Airplane Configuration Having a Wing With 40 Degrees of Sweepback and an Aspect Ratio of 10

Zero-Lift Drag of a Series of Bomb Shapes at Mach Numbers From 0.60 to 1.10

The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselage-Store Configurations 5: Swept-Wing Heavy-Bomber Configuration With Large Store (Nacelle). Mach Number 2.01

Acoustics of a Nonhomogeneous Moving Medium

Investigation of Lateral Control Near the Stall: Analysis for Required Longitudinal Trim Characteristics and Discussion of Design Variables

Performance of Pentaborane, Pentaborane - JP-4 Fuel Mixtures, and Trimethylborate Azeotrope Fuel in a Full-Scale Turbojet Engine

Wind-Tunnel Measurements of Wing Buffeting on 1/16-Scale Model of Douglas D-558-II Research Airplane

A Brief Investigation of the Effect of Waves on the Take-Off Resistance of a Seaplane

Conversion of Inviscid Normal-Force Coefficients in Helium to Equivalent Coefficients in Air for Simple Shapes at Hypersonic Speeds

Crash Injury

Effect of Pressure on the Spontaneous Ignition Temperature of Liquid Fuels

Effect of Blade-Section Camber on Aerodynamic Characteristics of Full-Scale Supersonic-Type Propellers at Mach Numbers to 1.04

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