Longitudinal motions of aircraft involving high angles of attack /

Effect of a rotating propeller on the separation angle of attack and distortion in ducted propeller inlets /
Published: (1992)

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

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

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)

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

Investigation of wake characteristics of a 0012 airfoil section : test no. 8228 /
by: Landrum, D. B. (David Brian), 1962-
Published: (1982)

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)

Determination of corrections to flow direction sensor measurements over an angle-of-attack range from 0⁰ to 85⁰ /
by: Moul, Thomas M.
Published: (1985)

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

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

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)

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

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

Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack /
by: Iliff, Kenneth W., et al.
Published: (1997)

Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes /
by: Nowak, Robert J., et al.
Published: (1985)

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

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)

A contribution to the theory of aircraft response in rolling manoeuvres : including inertia cross-coupling effects /
by: Thomas, H. H. B. M.
Published: (1964)

A scheme of notation and nomenclature for aircraft dynamics and associated aerodynamics /
by: Hopkin, H. R.
Published: (1970)

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

Angles are easy as pie /
by: Froman, Robert, 1917-
Published: (1975)

Angle modulation : the theory of system assessment /
by: Roberts, J. H.
Published: (1977)

An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft /
by: Steenken, William G.
Published: (1997)

Notes on the analysis of stability in accelerated motion /
by: Gates, S. B.
Published: (1965)

A wind tunnel investigation of the longitudinal and lateral aerodynamic characteristics of a canard aircraft model ; Pt. I. Tests at M = 1.40 and M = 2.02 /
by: Watts, P. E.
Published: (1962)

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

The unsteady forces on finite wings in transient motion /
by: Dore, Barrie Dennis
Published: (1967)

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

Measurement of aerodynamic heating on the nose of a delta aircraft at speeds up to M = 1.65 /
by: Nethaway, J. E.
Published: (1962)

Elevator flutter involving two tabs : by E. G. Broadbent and Mary Clarke.
by: Broadbent, E. G.
Published: (1961)

An experimental investigation of the subsonic longitudinal characteristics of five slender-wing models with gothic planforms /
by: Kirkpatrick, D. L. I.
Published: (1973)

Small angle scattering.
Published: (2022)

Whirl of an aircraft power-plant installation and its interaction with the flutter motion of a flexible wing /
by: Smith, G. E. (Gregory E.)
Published: (1968)

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

The test performance of highly loaded turbine stages designed for high preasure ratio /
by: Johnston, I. H.
Published: (1962)

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