An over-the-rotor liner investigation with configurations enabled by additive manufacturing /

Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle /
by: Lamb, Milton
Published: (1985)

Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle /
by: Lamb, Milton
Published: (1985)

Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds /
by: Mack, Robert J.
Published: (1999)

Computational aerodynamic simulations of a 1215 ft/sec tip speed transonic fan system model for acoustic methods assessment and development /
by: Tweedt, Daniel L. (Daniel Lawrence)
Published: (2014)

Open rotor aeroacoustic modelling /
by: Envia, Edmane
Published: (2012)

Computational aerodynamic simulations of an 840 ft/sec tip speed advanced ducted propulsor fan system model for acoustic methods assessment and development /
by: Tweedt, Daniel L. (Daniel Lawrence)
Published: (2014)

The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor /
by: Bozak, Richard F., et al.
Published: (2013)

Empennage noise shielding benefits for an open rotor transport /
by: Berton, Jeffrey J.
Published: (2012)

Tones encountered with a coannular nozzle and a method for their suppression /
by: Zaman, K. B. M. Q. (Khairul B. M. Q.)
Published: (2017)

Recent improvements to the Acoustical Testing Laboratory at the NASA Glenn Research Center /
by: Podboy, Devin M.
Published: (2014)

Advanced nacelle acoustic lining concepts development /
Published: (2002)

Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes /
by: Sutliff, Daniel L. (Daniel Linden), 1962-, et al.
Published: (2014)

Commercial cargo derivative study of the advanced hybrid wing body configuration with over-wing engine nacelles /
by: Hooker, John R., et al.
Published: (2017)

Pratt & Whitney/Boeing engine validation of noise reduction concepts : final report for NASA contract NAS3-97144.
by: Bock, Larry A.
Published: (2014)

Space station reference and configuration description /
Published: (1984)

Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /
by: Lamb, Milton, et al.
Published: (1987)

An experimental investigation of propfan installations on an unsewpt supercritical wing at transonic Mach numbers /
by: Bartlett, Glynn R.
Published: (1985)

Adaptive back sheet material for acoustics liner applications--ARMD Seedling Fund phase I final report /
by: Gerhold, Carl H., et al.
Published: (2014)

Finite difference time marching in the frequency domain : a parabolic formulation for aircraft acoustic nacelle design /
by: Baumeister, Kenneth J., et al.
Published: (1996)

An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts /
by: Mack, Robert J.
Published: (2005)

Investigation of "6X" scramjet inlet configurations /
by: Alter, Stephen J.
Published: (2012)

Full-scale turbofan engine noise-source separation using a four-signal method /
by: Hultgren, Lennart S. (Lennart Sven), et al.
Published: (2016)

Prediction of the aero-acoustic performance of open rotors /
by: Van Zante, Dale E., et al.
Published: (2014)

Analysis of NLR configurations using OCM for pilot modeling.
by: Drajeske, M. H.
Published: (1987)

Compressive testing of stitched frame and stringer alternate configurations /
by: Leone, Frank A., et al.
Published: (2016)

Analysis of NLR configurations using OCM for pilot modeling.
by: Drajeske, M. H.
Published: (1987)

Economic evaluation of flying-qualities design criteria for a transport configured with relaxed static stability /
by: Sliwa, Steven M.
Published: (1980)

Study for prediction of rotor/wake/fuselage interference /
by: Clark, D. R.
Published: (1985)

Experimental and theoretical study of flow fields around ducted-nacelle models /
by: Mack, Robert J.
Published: (1998)

Performance predictions for an SSME configuration with an enlarged throat /
by: Nickerson, G. R.
Published: (1985)

Benefit assessment for metroplex tactical runway configuration management (mTRCM) in a simulated environment /
by: Phojanamongkolkij, Nipa
Published: (2015)

Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight /
by: Berry, John D.
Published: (1997)

Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D /
by: Rumsey, C. L. (Christopher Lockwood), 1961-
Published: (2001)

Interactive calculation procedures for mixed compression inlets /
by: Reshotko, Eli
Published: (1983)

Full potential methods for analysis/design of complex aerospace configurations /
by: Shankar, Vijaya, et al.
Published: (1986)

PRSEUS acoustic panel fabrication /
by: Velicki, Alex
Published: (2011)