Cover Image

Light airplane crash tests at three pitch angles/

Main Author:	Vaughan, Victor L.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Other Authors:	Alfaro-Bou, Emilio
Format:	Book
Language:	English
Published:	Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1979
Series:	NASA technical paper 1481
Subjects:	Stability of airplanes > Testing Airplanes > Testing Pitching (Aerodynamics)

Similar Items

Light airplane crash tests at three flight-path angles/
by: Castle, Claude B.
Published: (1978)

Light airplane crash tests at three rolls angles/
by: Castle, Claude B.
Published: (1979)

Light airplane crash test at impact velocities of 13 and 27 m/sec/
by: Alfaro-Bou, Emilio
Published: (1977)

Crash tests of four identical high-wing single-engine airplanes/
by: Vaughan, Victor L.
Published: (1980)

Flight evaluation of a spoiler roll control system on a light twin-engine airplane/
by: Kohlman, David L., 1937-
Published: (1978)

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

Airplane flight dynamics and automatic flight controls /
by: Roskam, Jan
Published: (2003)

Similitude requirements and scaling relationships as applied to model testing/
by: Wolowicz, Chester H.
Published: (1979)

Theroetical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack/
by: Luckring, James M.
Published: (1977)

Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack/
by: Larson, Terry J.
Published: (1987)

Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model/
by: Capone, Francis J.
Published: (1980)

Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps/
by: Yip, Long P.
Published: (1987)

Measurement of the handling characteristics of two light airplanes/
Published: (1980)

Crash tests of four low-wing twin-engine airplanes with truss-reinforced fuselage structure/
by: Williams, M. Susan
Published: (1982)

Phugoid characteristics of YF-12 airplane with variable-geometry inlets obtained in flight tests at a Mach number of 2.9/
by: Powers, Bruce G.
Published: (1977)

Effects of control inputs on the estimation of stability and control parameters of a light airplane/
by: Cannaday, Robert L.
Published: (1977)

Application of a performance modeling technique to an airplane with variable sweep wings/
by: Redin, Paul C.
Published: (1981)

Stability and control of airplanes and helicopters/
by: Seckel, Edward
Published: (1964)

Design of integrated pitch axis for autopilot/autothrottle and integrated lateral axis for autopilot/yaw damper for NASA TSRV airplane using integral LQG methodology/
Published: (1990)

Performance, stability, dynamics, and control of airplanes
by: Pamadi, Bandu N., 1945-
Published: (2004)

Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)/
by: Hassell, James L.
Published: (1980)

The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane/
by: Stephenson, Jack D. 1922-
Published: (1983)

Estimation of attainable leading-edge thrust for wings at subsonic and supersonic speeds/
by: Carlson, Harry W.
Published: (1979)

Supersonic aerodynamic characteristics of canard, tailless and aft-tail configurations for two planforms/
by: Covell, Peter F.
Published: (1985)

Impact dynamics research facility for full-scale aircraft crash testing/
by: Vaughan, Victor L.
Published: (1976)

A throat-bypass stability-bleed system using relief valves to increase the transient stability of a mixed-compression inlet/
by: Neiner, George H.
Published: (1979)

Exploratory study of the effects of wing-leading-edge modifications on the stall/spin behavior of a light general aviation airplane/
Published: (1979)

Span reduction effects on flutter characteristics of arrow-wing supersonic transport configurations/
by: Keller, Donald F.
Published: (1991)

The effectiveness of vane-aileron excitation in the experimental determination of flutter speed by parameter identification/
by: Nissim, E.
Published: (1990)

Lateral aerodynamic parameters extracted from light data for the F-8C airplane in maneuvering flight/
by: Suit, William T. 1937-
Published: (1977)

Summary of flight tests to determine the spin and controllability characteristics of a remotely piloted, large-scale (3/8) fighter airplane model/
by: Holleman, Euclid C.
Published: (1976)

An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90/
by: Re, Richard J.
Published: (1977)

Precision controllability of the FY-17 airplane/
by: Sisk, Thomas R.
Published: (1980)

Loading tests of a wing structure for a hypersonic aircraft/
by: Fields, Roger A.
Published: (1980)

Procedures for the design of low-pitching-moment airfoils/
by: Barger, Raymond L.
Published: (1975)

Flight tests of the Digital Integrated Automatic Landing System (DIALS)/
by: Halyo, Nesim
Published: (1984)

Large-scale wind-tunnel tests of inverting flaps on a STOL utility aircraft model/
by: Feistel, Terrell W.
Published: (1980)

Rotary-balance testing for aircraft dynamics= Les essais sur balance rotative pour l'etude de la dynamique du vol de l'avion/
Published: (1990)

Friction and wear behavior of aluminum and composite airplane skins/
by: Jackson, Karen E.
Published: (1984)

Natural laminar flow experiments on modern airplane surfaces/
by: Holmes, Bruce J.
Published: (1984)

Cannot write session to /tmp/vufind_sessions/sess_vr1vdh7hpdi0p9jdgnit43dnk2