Determination of corrections to flow direction sensor measurements over an angle-of-attack range from 0⁰ to 85⁰ /

STEP and STEPSPL--computer programs for aerodynamic model structure determination and parameter estimation /
by: Batterson, James G.
Published: (1986)

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

Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack /
by: Nallasamy, M.
Published: (1989)

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)

Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove /
by: Bui, Trong T.
Published: (2014)

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)

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)

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

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

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)

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

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)

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

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

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)

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

Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade /
by: McVetta, Ashlie B., et al.
Published: (2013)

Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields /
by: Erickson, Gary E.
Published: (2010)

Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads /
by: Batina, John T.
Published: (1985)

Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers /
by: Boyle, Robert J.
Published: (1998)

Advanced noise control fan aerodynamic performance /
by: Bozak, Richard F., Jr
Published: (2009)

Estimates for the aerodynamic coefficients of ringsail and disk-gap-band parachutes operating on Mars /
by: Cross, John R., et al.
Published: (2017)

An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies /
by: Brykina, Irina G., et al.
Published: (1998)

Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes /
by: Bowman, James S. (James Scarboro), 1924-
Published: (1989)

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)

Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique /
by: Erickson, Gary E.
Published: (2013)

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)

Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade /
by: McVetta, Ashlie B., et al.
Published: (2014)

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

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

Broadband shock noise in internally-mixed dual-stream jets /
by: Bridges, James E.
Published: (2009)

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

Numerical procedure for three-dimensional hypersonic viscous flow over aerobrake configuration /
by: Li, Chien-peng
Published: (1985)

The effects of pressure sensor acoustics on airdata derived from a high-angle-of-attack flush airdata sensing (HI-FADS) system /
by: Whitmore, Stephen A.
Published: (1991)

Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰ /
by: Spearman, M. Leroy
Published: (1985)