Cover Image

Subsonic stability and control derivatives for an unpowered, remotely piloted 3/8-scale F-15 airplane model obtained from flight tests/

Main Author:	Iliff, Kenneth W.
Corporate Authors:	United States National Aeronautics and Space Administration, Flight Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Maine, Richard E., Shafer, Mary F.
Format:	Book
Language:	English
Published:	Washington: NASA, 1976
Series:	NASA technical note 8136
Subjects:	Eagle (Jet fighter plane) > Models > Testing Stability of airplanes Airplanes > Control systems

Similar Items

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)

Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane/
by: Webb, Lannie D.
Published: (1984)

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)

Simulator study of the effectiveness of an automatic control system designed to improve the high-angle-of-attack characteristics of a fighter airplane/
by: Gilbert, William P.
Published: (1976)

Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane/
by: Kurtenbach, Frank J.
Published: (1981)

Extraction from flight data of longitudinal aerodynamic coefficients in maneuvering flight for F-8C aircraft/
by: Suit, William T. 1937-
Published: (1975)

Flight-determined derivatives and dyanmic characteristics for the HL-10 lifting body vehicle at subsonic and transonic Mach numbers/
by: Strutz, Larry W.
Published: (1972)

Analysis of rotary balance data for the F-15 airplane including the effect of conformal fuel tanks/
by: Barnhart, Billy
Published: (1982)

Flight-determined stability and control derivatives for the F-111 TACT research aircraft/
by: Sim, Alex G.
Published: (1978)

Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47/
by: Capone, Francis J.
Published: (1987)

Effects of fuselage forebody geometry on low-speed lateral-directional characteristics of twin-tail fighter model at high angles of attack/
by: Carr, Peter C.
Published: (1979)

A case study on the F-16 fly-by-wire flight control system
by: Droste, Carl S.
Published: (1985)

Description and flight test results of the NASA F-8 digital fly-by-wire control system : a collection of papers from the NASA Symposium on Advanced Control Technology, Los Angeles, Calif., July 9-11, 1974 /
Published: (1975)

Velocity field of a round jet in a cross flow for various jet injection angles and velocity ratios/
by: Fearn, Richard L.
Published: (1979)

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

Simulator study of stall/post-stall characteristics of a fighter airplane with longitudinal static stability/
Published: (1979)

Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration/
by: Paulson, John W.
Published: (1984)

Analysis of longitudinal pilot-induced oscillati0on tendencies of YF-12 aircraft/
by: Smith, John W.
Published: (1975)

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

Wind-tunnel free-flight investigation of a model of a spin-resistant fighter configuration/
by: Grafton, Sue B.
Published: (1974)

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

Impact study on the use of JET A fuel in military aircraft during operatios in Europe : etude de l' impact de l' utilization du carburant JET A par les avions militaires lors des operations en Europe /
by: Batchelor, Graham
Published: (1997)

Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane/
by: Friend, Edward L.
Published: (1978)

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

Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter/
Published: (1983)

The jet V/STOL Harrier an evolutionary revolution in tactical air power /
Published: (1978)

Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards/
by: Robins, A. Warner
Published: (1979)

Advanced aircraft design conceptual design, technology and optimization of subsonic civil airplanes /
by: Torenbeek, Egbert.
Published: (2013)

Control definition study for advanced vehicles/
Published: (1983)

Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration/
by: Satran, Dale R.
Published: (1986)

Flight effects on noise generated by the JT8D engine with inverted primary/fan flow as measured in the NASA-Ames 40- by 80-foot wind tunnel/
by: Strout, Frank G.
Published: (1978)

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

Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model/
by: Reubush, David E.
Published: (1975)

Manoeuvre limitations of combat aircraft
Published: (1979)

A computer technique for detailed analysis of mission radius and maneuverability characteristics of fighter aircraft/
by: Foss, Willard E.
Published: (1981)

Effect of fuselage upwash on the supersonic longitudinal aerodynamic characteristics of two fighter configurations/
by: Wood, Richard M.
Published: (1984)

Flight effects on noise generated by the JT8D-17 engine in a quiet nacelle and a conventional nacelle as measured in the NASA-Ames 40-by 80-foot wind tunnel : Summary report /
by: Strout, Frank G.
Published: (1976)

Flight stability and automatic control /
by: Nelson, Robert C., 1942-
Published: (1998)

New methods and results for quantification of lightning-aircraft electrodynamics/
Published: (1987)

Landing practices of general aviation pilots in single-engine light airplanes/
Published: (1976)

Cannot write session to /tmp/vufind_sessions/sess_fk51kepcn86fvsn9sumskqkdn2