Pseudosteady-state analysis of nonlinear aircraft maneuvers /

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)

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

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

High-Alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle /
by: Wichman, Keith D.
Published: (1996)

Lateral-directional eigenvector flying qualities guidelines for high performance aircraft /
by: Davidson, John B., et al.
Published: (1996)

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)

Rotary wing aircraft scientific and technical publications of NASA between 1970 and 1982 /
Published: (1982)

Nonlinear aerodynamic modeling from flight data using advanced piloted maneuvers and fuzzy logic /
by: Brandon, Jay M., et al.
Published: (2012)

Investigation of piloting aids for manual control of hypersonic maneuvers /
by: Raney, David L.
Published: (1995)

AMT-200S motor glider parameter and performance estimation /
by: Taylor, Brian R.
Published: (2011)

Assessment of aerodynamic performance of V/STOL and STOVL fighter aircraft /
by: Nelms, W. P.
Published: (1984)

Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration /
by: Kemmerly, Guy T.
Published: (1990)

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

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft /
by: Steenken, William G.
Published: (1999)

Maneuver acoustic flight test of the Bell 430 helicopter data report /
by: Watts, Michael E.
Published: (2014)

Helistat simulation studies /
by: Tischler, Mark B. (Mark Brian), 1957-, et al.
Published: (1982)

Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV /
by: Fisher, David F., et al.
Published: (1996)

A flight-test methodology for identification of an aerodynamic model for a V/STOL aircraft /
by: Bach, Ralph E.
Published: (1988)

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

Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods /
by: Freudinger, Lawrence C.
Published: (1989)

The design of sport and touring aircraft /
by: Eppler, R.
Published: (1984)

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

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

Acoustic performance of the GEAE UPS research fan in the NASA Glenn 9- by 15-foot low-speed wind tunnel /
by: Woodward, Richard P.
Published: (2012)

Development and implementation of a model-driven envelope protection system for in-flight ice contamination /
Published: (2011)

An overview of three approaches to multidisciplinary aeropropulsion simulations /
by: Lawrence, Charles, 1957-
Published: (1997)

Candidate control design metrics for an agile fighter /
by: Murphy, Patrick C.
Published: (1991)

Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover /
by: Franklin, James A., et al.
Published: (1996)

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

Review of the Aerodynamic Acceptance Test and application to anti-icing fluids testing in the NRC propulsion and icing wind tunnel /
by: Broeren, Andy P., et al.
Published: (2012)

A wind tunnel study of icing effects on a business jet airfoil /
Published: (2003)

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

Technology assessment for large vertical-lift transport tiltrotors /
by: Germanowski, Peter J.
Published: (2010)

Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at supersonic speeds /
by: Kim, Hyun D.
Published: (2001)

Synthesis from design requirements of a hybrid system for transport aircraft longitudinal control /
by: Hynes, Charles S., et al.
Published: (2007)