TRAIL - Technical Report Archive and Image Library

Effects of wing elasticity on the aerodynamic characteristics of a 45 degree sweptback-wing-fuselage combination measured in the Langley 8-foot transonic tunnel

The effects of oscillation amplitude and frequency on the experimental damping in pitch of a triangular wing having an aspect ratio of 4

Effects of plan form, airfoil section, and angle of attack on the pressures along the base of blunt-trailing-edge wings at Mach numbers of 1.41, 1.62, and 1.96

Effects of horizontal-tail position and aspect ratio on low-speed static longitudinal stability and control characteristics of a 60 degree triangular-wing model having twin triangular all-movable tails

Effects of finite span on the section characteristics of two 45 degree swept-back wings of aspect ratio 6

Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a high-aspect-ratio bomber model with a sweptback-wing fighter model attached to each wing tip

A summary and analysis of the low-speed longitudinal characteristics of swept wings at high Reynolds number

A transonic wind-tunnel investigation of the effects of nacelle shape and position on the aerodynamic characteristics of two 47 degree sweptback wing-body configurations

A transonic wind-tunnel investigation of the characteristics of a twisted and cambered 45 degree sweptback wing-fuselage configuration

Summary of methods for calculating dynamic lateral stability and response and for estimating aerodynamic stability derivatives

Altitude performance investigation of single- and double-annular turbojet-engine combustors with various size fuel nozzles

Altitude investigation of three flame-holder and fuel-systems configurations in a short converging afterburner on a turbojet engine

The transonic characteristics of 38 cambered rectangular wings of varying aspect ratio and thickness as determined by the transonic-bump technique

Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds : aspect-ratio series

Altitude performance of annular combustor type turbojet engine with JFC-2 fuel

Altitude performance investigation of two flame-holder and fuel-system configurations in short afterburner

Altitude wind tunnel investigation of high-temperature afterburners

Two-dimensional chord-wise load distributions at transonic speeds

An active particle diffusion theory of flame quenching for laminar flames

Transonic aerodynamic characteristics of three thin triangular wings and a trapezoidal wing, all of low aspect ratio

Low-speed lateral-control characteristics of an unswept wing with hexagonal airfoil sections and aspect ratio 2.5 equipped with spoilers and with sharp- and thickened-trailing-edge flap-type ailerons at a Reynolds number of 7.6 x 10(exp 6)

Low-speed longitudinal characteristics of a 45 degrees sweptback wing of aspect ratio 8 with high-lift and stall-control devices at Reynolds numbers from 1,500,000 to 4,800,000

Low speed stability characteristics of a complete model with a wing of W plan form

Low-speed static longitudinal stability and control characteristics of 60 degree triangular-wing and modified 60 degree triangular-wing models having half-delta and half-diamond tip controls

Low-speed static longitudinal and lateral stability characteristics of a model with leading-edge chord-extensions incorporated on a 40 degree sweptback circular-arc wing of aspect ratio 4 and taper ratio 0.50

Low-speed tests of a free-to-yaw model in two wind tunnels of different turbulence

An investigation of the subsonic speed range of a full-span and a semispan model of a plane wing and of a cambered and twisted wing, all having 45 degrees of sweepback

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

Keyword Search

Published Year

Subject

Author