Nacelles

68 books
NASA acoustically treated nacelle programLangley Research Center
⏱ 2h 45m

NASA acoustically treated nacelle program

Langley Research Center

1969165 pp.
Resistance tests of models of three flying-boat hulls with a length-beam ration of 10.5Langley Aeronautical Laboratory
⏱ 48m

Resistance tests of models of three flying-boat hulls with a length-beam ration of 10.5

Langley Aeronautical Laboratory

194548 pp.
Nacelle Aerodynamic and Inertial Loads (NAIL) projectUnknown Author

Nacelle Aerodynamic and Inertial Loads (NAIL) project

Unknown Author

1982No page data
Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport modelOdis C. Pendergraft
⏱ 1h 45m

Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport model

Odis C. Pendergraft

1992105 pp.
Nacelle Aerodynamic and Inertial Loads (NAIL) projectUnknown Author

Nacelle Aerodynamic and Inertial Loads (NAIL) project

Unknown Author

1982No page data
Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transportWilliam Kelly Abeyounis

Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport

William Kelly Abeyounis

1990No page data
Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelleMilton Lamb

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

Milton Lamb

1985No page data
Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wingEdwin E. Lee
⏱ 2h 22m

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

Edwin E. Lee

1985142 pp.
Effects of wing and nacelle modifications on drag and wake characteristics of a bomber-type airplane modelLangley Aeronautical Laboratory
⏱ 2h 56m

Effects of wing and nacelle modifications on drag and wake characteristics of a bomber-type airplane model

Langley Aeronautical Laboratory

1945176 pp.
Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport airplaneWilliam Kelly Abeyounis
⏱ 1h 35m

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

William Kelly Abeyounis

199095 pp.
Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport modelUnknown Author

Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport model

Unknown Author

1992No page data
B-1 AFT nacelle flow visualization studyJames L. Gunter

B-1 AFT nacelle flow visualization study

James L. Gunter

1975No page data
Effect of nacelles on aerodynamic characteristics of an executive-jet model with simulated, partial-chord, laminar-flow-control wing gloveRichard L. Campbell
⏱ 1h 41m

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

Richard L. Campbell

1982101 pp.
Analysis of results from wind tunnel tests of inlets for an advanced turboprop nacelle installationJ. P. Hancock

Analysis of results from wind tunnel tests of inlets for an advanced turboprop nacelle installation

J. P. Hancock

1989No page data
Supersonic flow visualization of a nacelle in close proximity to a simulated wingKasim Biber

Supersonic flow visualization of a nacelle in close proximity to a simulated wing

Kasim Biber

1993No page data
Study to improve airframe turbine engine rotor blade containmentC. O. Gunderson
⏱ 3h 32m

Study to improve airframe turbine engine rotor blade containment

C. O. Gunderson

1977212 pp.
Determination of jet-boundary corrections to cowling-flap-outlet pressures by an electrical analogy methodLangley Aeronautical Laboratory
⏱ 38m

Determination of jet-boundary corrections to cowling-flap-outlet pressures by an electrical analogy method

Langley Aeronautical Laboratory

194438 pp.
Advanced nacelle acoustic lining concepts developmentUnknown Author

Advanced nacelle acoustic lining concepts development

Unknown Author

2002No page data
Tests on an engine installation for a slender gothic wing at M-1.82R. T. Griffiths
⏱ 21m

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

R. T. Griffiths

196721 pp.
Drag measurements of an axisymmetric nacelle mounted on a flat plate at supersonic speedsJeffrey D. Flamm
⏱ 32m

Drag measurements of an axisymmetric nacelle mounted on a flat plate at supersonic speeds

Jeffrey D. Flamm

199532 pp.
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