Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft /

Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds /
by: Erickson, Gary E.
Published: (2013)

Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing /
by: Laflin, Brenda E. Gile, et al.
Published: (1997)

Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed /
by: Erickson, Gary E.
Published: (2017)

Pseudosteady-state analysis of nonlinear aircraft maneuvers /
by: Young, John W. (John Worth), 1934-, et al.
Published: (1980)

Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack /
by: Walsh, Kevin R.
Published: (1997)

Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flights /
by: Moes, Timothy R.
Published: (1991)

Computational study of the impact of unsteadiness on the aerodynamic performance of a variable-speed power turbine /
by: Welch, Gerard E.
Published: (2012)

Development of the Transport Class Model (TCM) aircraft simulation from a sub-scale Generic Transport Model (GTM) simulation /
by: Hueschen, Richard M.
Published: (2011)

Flight test of an adaptive configuration optimization system for transport aircraft /
by: Gilyard, Glenn B., et al.
Published: (1999)

Low-speed stability-and-control and ground-effects measurements on the industry reference high speed civil transport /
by: Kennerly, Guy T.
Published: (1999)

Exploratory low-speed wind-tunnel study of concepts designed to improve aircraft stability and control at high angles of attack /
by: Hahne, David E. (David Edgar)
Published: (1985)

In-flight flow visualization results from the X-29A aircraft at high angles of attack /
by: Del Frate, John H., et al.
Published: (1992)

Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees /
by: Prabhu, Ramadas K.
Published: (2001)

Design guide for aerodynamics testing of Earth and planetary entry vehicles in a ballistic range /
by: Bogdanoff, D. W. (David W.)
Published: (2017)

Far-field acoustic power level and performance analyses of F31/A31 open rotor model at simulated scaled takeoff, nominal takeoff, and approach conditions, technical report I /
by: Sree, Dave
Published: (2015)

Review of research on angle-of-attack indicator effectiveness /
by: Le Vie, Lisa R.
Published: (2014)

Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers /
by: Stoliker, Patrick C., et al.
Published: (1996)

Local flow conditions for proplusion experiments on the F-15B Propulsion Flight Test Fixture /
by: Vachon, Michael J.
Published: (2005)

Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
by: Pittman, Jimmy L., et al.
Published: (1980)

Subsonic Ultra Green Aircraft Research : phase I final report /
by: Bradley, Marty K.
Published: (2011)

Subsonic dynamics of stardust sample return capsule /
by: Mitcheltree, Robert A. (Robert Alan), 1961-, et al.
Published: (1997)

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 /
by: Re, Richard J., et al.
Published: (1996)

Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment /
by: Greer, Donald, 1896-
Published: (1999)

Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft /
by: Klein, Vladislav
Published: (1997)

Extended parametric representation of compressor fans and turbines /
by: Converse, George L.
Published: (1984)

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds /
Published: (2001)

First-order altitude effects on the cruise efficiency of subsonic transport aircraft /
by: Guynn, Mark D.
Published: (2011)

F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack /
by: Yuhas, Andrew J.
Published: (1997)

Experimental effects of wing location on wing-body pressures at supersonic speeds /
by: Allen, Jerry M., et al.
Published: (1993)

The F/A-18 high-angle-of-attack ground-to-flight correlation, lessons learned /
by: Banks, Daniel W.
Published: (1997)

An overview of NASA's Subsonic Research Aircraft Testbed (SCRAT) /
by: Baumann, Ethan, et al.
Published: (2013)

Method for the prediction of the installation aerodynamics of a propfan at subsonic speeds : user manual /
by: Chandrasekaran, B., 1942-
Published: (1986)

Application of variable-gain output feedback for high-alpha control /
by: Ostroff, Aaron J.
Published: (1990)

Optimal pitch thrust-vector angle and benefits for all flight regimes /
by: Gilyard, Glenn B., et al.
Published: (2000)

Subsonic investigation of a leading-edge boundary layer control suction system on a high-speed civil transport configuration /
by: Campbell, Bryan A.
Published: (1999)

Aeromechanical stability of a hingeless rotor in hover and forward flight : analysis and wind tunnel tests /
by: Yeager, William T., et al.
Published: (1983)