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Free-Spinning-Tunnel Investigation of a 1/25-Scale Model of the McDonnell F3H-2N Airplane

Comparison of Mechanical Properties of Flat Sheets, Molded Shapes, and Postformed Shapes of Cotton-Fabric Phenolic Laminates

Component Performance Investigation of J71 Experimental Turbine 9 - Effect of First-Stator Adjustment;Internal Flow Conditions of J71-97 Turbine With 87-Percent-Design Stator Area

Compressibility Effects on a Hovering Helicopter Rotor Having an NACA 0018 Root Airfoil Tapering to an NACA 0012 Tip Airfoil

Comparison and Evaluation of Two Model Techniques Used in Predicting Bomb-Release Motions

Design and Engine Evaluation of a Semistrut Corrugated Air-Cooled Turbine Blade for Operation at a Tip Speed of 1300 Feet Per Second

Design and Investigation of a Transonic Axial-Flow Compressor Rotor With an Inlet Hub-Tip Radius Ratio of Essentially Zero

Design and Performance of Fuel Control for Aircraft Hydrogen Fuel System

Aerodynamic Heating and Boundary-Layer Transition on a 1/10-Power Nose Shape in Free Flight at Mach Numbers Up to 6.7 and Free-Stream Reynolds Numbers Up To 16 x 10(Exp 6)

Aerodynamic Characteristics of Missile Configurations With Wings of Low Aspect Ratio for Various Combinations of Forebodies, Afterbodies, and Nose Shapes for Combined Angles of Attack and Sideslip at a Mach Number of 2.01

An Analytical Study of the Effects of Increasing Fin Chord on the Lift and Longitudinal Stability Characteristics of Constant-Span Fin-Body Combinations of Fineness Ratio 14

Aerodynamic Characteristics of a Model of an Escape Capsule for a Supersonic Bomber-Type Airplane at a Mach Number of 2.49

An Air-Borne Target Simulator for Use With Scope-Presentation Type Fire-Control Systems

Airplane Measurements of Atmospheric Turbulence for Altitudes Between 20,000 and 55,000 Feet Over the Western Part of the United States

Analysis of Wing Loads on a Flexible Swept-Wing Jet Bomber During Push-Pull Maneuvers

Measurement of Static Pressure on Aircraft

Measurement of Static Forces on Internally Carried Bombs of Three Fineness Ratios in Flow Field of a Swept-Wing Fighter-Bomber Configuration at a Mach Number of 1.61 With Illustrative Drop-Path Calculations

A Method of Computing the Transient Temperature of Thick Walls From Arbitrary Variation of Adiabatic-Wall Temperature and Heat-Transfer Coefficient

A Method of Computing the Transient Temperature of Thick Walls From Arbitrary Variation of Adiabatic-Wall Temperature and Heat-Transfer Coefficient

A Flight Investigation to Determine the Effectiveness of Mach Number 1.0, 1.2, and 1.41 Fuselage Indentations for Reducing the Pressure Drag of a 45 Degree Sweptback Wing Configuration at Transonic and Low Supersonic Speeds

Flight Investigation of Factors Affecting the Choice of Minimum Approach Speed for Carrier-Type Landings of a Swept-Wing Jet Fighter Airplane

Flight Investigation of a Supersonic Propeller on a Propeller Research Vehicle at Mach Numbers to 1.01

High-Pressure Blowing Over Flap and Wing Leading Edge of a Thin Large-Scale 49 Degree Swept Wing-Body-Tail Configuration in Combination With a Drooped Nose and a Nose With a Radius Increase

Low-Speed Cascade Investigation of Thin Low-Camber Naca 65-Series Blade Sections at High Inlet Angles

Measurement of Aerodynamic Heat Transfer to a Deflected Trailing-Edge Flap on a Delta Fin in Free Flight at Mach Numbers From 1.5 to 2.6

Lateral Stability Investigation at Mach Numbers From 0.8 to 1.7 of Two Rocket-Boosted Models of an Airplane Configuration With a 45 Degree Swept Wing and a Low Horizontal Tail

Investigation of the Low-Speed Performance and Static Longitudinal Stability and Control Characteristics of a 60 Degree Delta-Wing-Body-Tail Combination With Blowing Over Trailing-Edge Flaps

Investigation of the Low-Speed Stability and Control Characteristics of a 1/7-Scale Model of the North American X-15 Airplane

Preliminary investigation of the altitude performance of pentaborane and a pentaborane : JP-4 blend in an experimental 9.5-inch-diameter tubular combustor

Ground Effects on the Longitudinal Characteristics of Two Models With Wings Having Low Aspect Ratio and Pointed Tips

Flutter Characteristics at Transonic Speeds of a 45 Degree Sweptback Wing With and Without Inboard Modifications at the Leading and Trailing Edges

Flutter and Divergence of Rectangular Wings of Very Low Aspect Ratio

Free-Flight Aerodynamic-Heating Data to a Mach Number of 15.5 on a Blunted Conical Nose With a Total Angle of 29 Degrees

Heat Transfer Measured on a Flat-Face Cylinder in Free Flight at Mach Numbers Up to 13.9

Horizontal-Tail Parameters as Determined From Flight-Test Tail Loads on a Flexible Swept-Wing Jet Bomber

A General System for Calculating Burning Rates of Particles and Drops and Comparison of Calculated Rates for Carbon, Boron, Magnesium, and Isooctane

Heat Transfer and Boundary-Layer Transition on a Highly Polished Hemisphere-Cone in Free Flight at Mach Numbers Up to 3.14 and Reynolds Numbers Up to 24 X 10(Exp 6)

Heat-Transfer and Pressure Distribution on Six Blunt Noses at a Mach Number of 2

Heat-Transfer and Pressure Measurements From a Flight Test of a 1/18-Scale Model of the Titan Intercontinental Ballistic Missile Up to a Mach Number of 3.95 and Reynolds Number Per Foot of 23 X 10(Exp 6): Coord. No. AF-AM-70

Free-Flight Determination of Boundary-Layer Transition and Heat Transfer for a Hemisphere-Cylinder at Mach Numbers to 5.6

Flight Performance of a 2.8 KS 8100 Cajun Solid-Propellant Rocket Motor

Flutter Investigation on the High Subsonic and Transonic Speed Range on Cantilever Delta-Wing Plan Forms With Leading-Edge Sweepback of 60 Degrees, 53 Degrees 8', and 45 Degrees

Investigation at Transonic Speeds of the Effects of Inlet-Lip Sweep on the Internal-Flow Characteristics of a Semielliptical Air Inlet With an Inlet-Lip Stagger of 30 Degrees

Investigation of a 0.6 Hub-Tip Radius-Ratio Transonic Turbine Designed for Secondary-Flow Study 1: Design and Experimental Performance of Standard Turbine

Investigation of a High-Performance Axial-Flow Compressor Transonic Inlet Rotor Designed for 37.5 Pounds Per Second Per Square Foot of Frontal Area: Detailed Blade-Element Performance

Calculated Effect of Some Airplane Handling Techniques on the Ground-Run Distance in Landing on Slippery Runways

A Low-Speed Investigation of the Magnus Effects on a Sting-Mounted Model of a Typical Mortar Shell

Annual Report of the National Advisory Committee for Aeronautics (42nd). Administrative Report Including Technical Report Nos. 1254 to 1295

Aerodynamic interference of slender wing-tail combinations

Aerodynamic Characteristics of a Circular Cylinder at Mach Number 6.86 and Angles of Attack Up to 90 Degrees


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