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A vector study of linearized supersonic flow applications to nonplanar problems

Investigation with an interferometer of the flow around a circular-arc airfoil at mach numbers between 0.6 and 0.9

Laminar boundary layer on cone in supersonic flow at large angle of attack

A probability analysis of the meteorological factors conducive to aircraft icing in the United States

Gust-response analysis of an airplane including wing bending flexibility

Displacement effect of a three-dimensional boundary layer

Some experiments on visualization of flow fields behind low-aspect-ratio wings by means of a tuft grid

Theoretical analyses to determine unbalanced trailing-edge controls having minimum hinge moments due to deflection at supersonic speeds

Experimental investigation of transition of a model helicopter rotor from hovering to vertical autorotation

Effects of Mach number variation between 0.07 and 0.34 and Reynolds number variation between 0.97 x 10(exp 6) and 8.10 x 10(exp 6) power on the maximum lift coefficient of a wing of NACA 64-210 airfoil sections

A comparison of the spanwise loading calculated by various methods with experimental loadings obtained on a 45 degrees sweptback wing of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)

Summary of stall-warning devices

flow studies in the vicinity of a modified flat-plate rectangular wing of aspect ratio 0.25

Measurements of temperature variations in the atmosphere near the tropopause with reference to airspeed calibration by the temperature method

A compressible-flow plotting device and its application to cascade flows

Boundary-layer development and skin friction at mach number 3.05

Altitude Investigation of Gas Temperature Distribution at Turbine of Three Similar Axial-Flow Turbojet Engines

Summary of Low-Lift Drag and Directional Stability Data from Rocket Models of the Douglas XF4D-1 Airplane with and without External Stores and Rocket Packets at Mach Numbers from 0.8 to 1.38: TED No. NACA DE-349

Altitude Starting Tests of a 1000-Pound-Thrust Solid-Propellant Rocket

Investigation of wear and friction properties under sliding conditions of some materials suitable for cages of rolling-contact bearings

Theoretical Investigation of the Effects of the Artificial-Feel System on the Maneuvering Characteristics of the F-89 Airplane

Analytical study of shimmy of airplane wheels

Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow

Airfoil profiles for minimum pressure drag at supersonic velocities -- general analysis with application to linearized supersonic flow

Preliminary air-flow and thrust calibrations of several conical Cooling-air ejectors with a primary to secondary temperature ratio of 1.0 I :diameter ratios of 1.21 and 1.10

Solubility of water in hydrocarbons

Performance characteristics at Mach numbers to 2.0 of various types of side inlets mounted on fuselage of proposed supersonic airplane IV : rectangular cowl inlets with two-dimensional compression ramps

Performance and operational characteristics of a python turbine-propeller engine at simulated altitude conditions / Carl L. Meyer and Lavern A. Johnson

Performance characteristics of canard-type missile with vertically mounted nacelle engines at Mach numbers 1.5 to 2.0

Performance characteristics at Mach numbers to 2.0 of various types of side inlets mounted on fuselage of proposed supersonic airplane 3: normal wedge inlet with semicircular cowl

Performance characteristics of canard-type missile with wing-mounted nacelle engines at Mach numbers 1.5 to 2.0

Recent data on controls

Some control considerations for ram-jet engines

Preliminary investigation of control characteristics at transonic speeds of a tapered 45 degree sweptback wing of aspect ratio 3 having a horn-balanced full-span control

Preliminary investigation of flow fluctuations during surge and blade row stall in axial-flow compressors / c Merle C. Huppert

Pressure recovery, drag, and subcritical stability characteristics of three conical supersonic diffusers at stream Mach numbers from 1.7 to 2.0

Pressure limits of flame propagation of pure hydrocarbon-air mixtures at reduced pressure

An approximation to the effect of geometric dihedral on the rolling moment due to sideslip for wings at transonic and supersonic speeds

An analysis of the effect of structural feedback on the flutter of a control surface having a power-boost system

Influence of a canard-type control surface on the internal and external performance characteristics of nacelle-mounted supersonic diffusers (conical centerbody) at a rearward body station for a Mach number of 2.0

Influence of fuselage-mounted rocket boosters on flow field at inlet and on diffuser performance of strut-mounted engine at Mach numbers of 1.8 and 2.0

Influence of fuselage and canard-type control surface on the flow field adjacent to a rearward fuselage station at a Mach number of 2.0 : data presentation

Hinge-moment and control-effectiveness characteristics of an outboard flap with an overhang nose balance on a tapered 35 degree sweptback wing of aspect ratio 4: transonic-bump method

Influence of a canard-type control surface on flow field in vicinity of symmetrical fuselage at Mach numbers 1.8 and 2.0

Forces and moments on pointed blunt-nosed bodies of revolution at Mach numbers from 2.75 to 5.00

The Ames supersonic free-flight wind tunnel

An analysis of the effect of a curved ramp on the take-off performance of catapult-launched airplanes

Empirical cooling correlation for an experimental afterburner with an annular cooling passage

Effect of inlet air and fuel parameters on smoking characteristics of a single tubular turbojet engine combustor

Force and pressure-recovery characteristics of a conical-type nose inlet operating at Mach numbers of 1.6 to 2.0 and at angles of attack to 9 degrees


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