Explore Books on
nacelles

Boundary-layer separation on isolated boattail nozzles

By William Kelly Abeyounis

Effect of underwing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane

By William Kelly Abeyounis

Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport

By Milton Lamb

B-1 AFT nacelle flow visualization study

By James L. Gunter

An installed nacelle design code using a multiblock Euler solver

By H. C. Chen

Installed nacelle drag-improvement tests of an M=0.8 turboprop transport configuration

By Alan D. Levin

XV-15 structural-acoustic data

By Karen H. Lyle

Hover in-ground-effect testing of a full-scale, tilt-nacelle V/STOL model

By James E. Eshleman

A grid-embedding transonic flow analysis computer program for wing/nacelle configurations

By Essam H. Atta

Design of 3-D nacelle near flat-plate wing using multiblock sensitivity analysis (ADOS)

By Mohamed E. Eleshaky

Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle

By Milton Lamb

Finite difference time marching in the frequency domain

By Kenneth J. Baumeister

Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft

By Michael A. Boles

Short Haul Civil Tiltrotor study in MIDAS

By Adolph Atencio

Experimental and theoretical study of flow fields around ducted-nacelle models

By Robert J. Mack

Effect of nacelles on aerodynamic characteristics of an executive-jet model with simulated, partial-chord, laminar-flow-control wing glove

By Richard L. Campbell

Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing

By Edwin E. Lee

Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration

By Lawrence E. Putnam

Effects of nacelle configuration/position on performance of subsonic transport

By L. H. Bangert

Hover test results of a small-scale twin-tilt nacelle model

By Susan B. Schmidt

Installed nacelle drag-improvement tests of an M=0.8 turboprop transport configuration

By Alan D Levin

Wind tunnel tests on a streamlined fan-lift nacelle

By James Ernest Hackett

Tests at M= 1.82 on an engine installation with boundary-layer diverter for a slender gothic wing

By R. T. Griffiths

Tests on an engine installation for a slender gothic wing at M-1.82

By R. T. Griffiths