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A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel

Tests of a small-scale NACA submerged inlet at transonic Mach numbers

An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2

Investigation of the NACA 4-(0)(03)-45 two-blade propeller at forward Mach numbers to 0.925

Investigation of a simple device for preventing separation due to shock and boundary-layer interaction

Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift

Investigation of an impulse axial-flow compressor rotor over a range of blade angles

Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing

Effects of Mach number up to 0.34 and Reynolds number up to 8,000,000 on the maximum lift coefficient of a wing of NACA 66-series airfoil sections

Flight calibration of four airspeed systems on a swept-wing airplane at Mach numbers up to 1.04 by the NACA radar-phototheodolite method

Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35©�, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method

Aerodynamic investigation at Mach number 1.92 of a rectangular wing and tail and body configuration and Its components

Performance of J33-A-27 Turbojet-Engine Compressor, II, Over - All Performance Characteristics of Modified Compressor at Equivalent Impeller Speeds from 6100 to 13,250 RPM

Static Longitudinal Stability of a Tandem-Coupled Bomber-Fighter Airplane Configuration Similar to One Proposed by Douglas Aircraft Company, Inc.

Static Longitudinal Stability of a Tandem-Coupled Bomber-Fighter Airplane Configuration Proposed by All American Airways, Inc.

Transonic Stability and Control Investigation of a 1/80-Scale Model of the Consolidated Vultee Skate 9 Seaplane, TED No. NACA DE 345: Transonic-Bump Method

Ditching Investigation of a 1/24-Scale Model of the Boeing B-47 Airplane

Preliminary Performance Data on Westinghouse Electronic Power Regulator Operating on J34-WE-32 Turbojet Engine in Altitude Wind Tunnel

Investigation of High-Subsonic Performance Characteristics of a 12 Degree 21-Inch Conical Diffuser, Including the Effects of Change in Inlet-Boundary-Layer Thickness

Tests of a Northrop XSSM-A-3 Missile in the Ames 40- by 80-Foot Wind Tunnel: Stability and Control

Calibration of Instruments for Measuring Wind Velocity and Direction

Investigation of Altitude Ignition, Acceleration, and Steady-State Operation with a Single Combustor of a J47 Turbojet Engine

Gust-Tunnel Investigation to Determine the Load at the Joint of a Coupled Airplane Configuration Encountering a Gust

General method and thermodynamic tables for computation of equilibrium composition and temperature of chemical reactions

Icing-protection requirements for reciprocating-engine induction systems

Flight experiences and tests on two airplanes with suction slots

Icing Characteristics and Anti-Icing Heat Requirements for Hollow and Ternally Modified Gas-Heated Inlet Guide Vanes

Analytical determination of local surface heat-transfer coefficients for cooled turbine blades from measured metal temperatures

Experimental and Analytical Study of Balanced-Diaphragm Fuel Distributors for Gas-Turbine Engines

Penetration of Air Jets Issuing from Circular, Square, and Elliptical Orifices Directed Perpendicularly to an Air Stream

Interpretation of boundary-layer pressure-rake data in flow with a detached shock

Fabrication and Properties of Hot-Pressed Molybdenum Disilicide

Investigation of frequency-response characteristics of engine speed for a typical turbine-propeller engine

Investigation of first stage of two-stage turbine designed for free-vortex flow

Investigation of fretting corrosion by microscopic observation

First-order theory for unsteady motion of thin wings at supersonic speeds

A numerical procedure for designing cascade blades with prescribed velocity distribution in incompressible potential flow

Friction and wear of hot-pressed bearing materials containing molybdenum disulfide

Interferometer corrections and measurements of laminar boundary layers in supersonic stream

Investigation of a NACA high-speed optical torquemeter

Investigation of a NACA high-speed strain-gage torquemeter

Investigation of properties of AISI type 310B alloy sheet at high temperatures

Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design

A method of calibrating airspeed installations on airplanes at transonic and supersonic speeds by use of temperature measurements

Method of calculating the lateral motions of aircraft based on the Laplace transform

A method of computing subsonic flows around given airfoils

The NACA oil-damped V-G recorder

Wind-tunnel investigation at low speed of a 45 degree sweptback untapered semispan wing of aspect ratio 1.59 equipped with various 25-percent chord plain flaps

Wind-tunnel investigation at low speed of an unswept untapered semispan wing of aspect ratio 3.13 equipped with various 25-percent-chord plain flaps

Wind-tunnel investigation at low speed of the lateral control characteristics of an unswept untapered semi-span wing of aspect ratio 3.13 equipped with various 25-percent-chord plain ailerons


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