Hoenlinger et al., 1980 - Google Patents
Active suppression of aircraft flutterHoenlinger et al., 1980
- Document ID
- 14566109347511881356
- Author
- Hoenlinger H
- Lotze A
- Publication year
- Publication venue
- International Council of the Aeronautical Sciences, Congress, 11 th, Lisbon, Portugal
External Links
- 230000001629 suppression 0 title description 2
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/008—Rotors tracking or balancing devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Hoenlinger et al. | Active suppression of aircraft flutter | |
Zarovsky et al. | Flight Investigation of a Roll-Stabilized Missile Configuration at Varying Angles of Attack at Mach Numbers Between 0.8 and 1.79 | |
Reed III et al. | Passive control of wing/store flutter | |
Barzda et al. | Test Results of Rotary-Wing Decelerator Feasibility Studies for Capsule Recovery Applications | |
Loy | Carefree handling and its applications to military helicopters and missions | |
MARSHALL | Determination of in-flight modal characteristics of a fighter type aircraft | |
DAVIS et al. | Controlling dynamic response in rough air | |
Hodge | FLIGHT DYNAMIC EVALUATION OF THE BULLPUP B MISSILE | |
Reed et al. | A comparison between transonic wind-tunnel and full-scale store separation characteristics. | |
Charwat | The Stability of Bodies of Revolution at Very High Mach Numbers | |
Whitbeck et al. | Optimal terrain-following feedback control for advanced cruise missiles[Final Report] | |
Barzda | Rotary Wing Decelerators | |
ONDA et al. | The concept of an unmanned flying vehicle at high altitude | |
LOCK et al. | Flight investigation of a structural mode control system for the XB-70 aircraft(Flight test of structural mode control system installed in XB-70 aircraft to determine effectiveness of system under turbulent conditions) | |
Crabill | Ascent problems of sounding rockets | |
GIROLAMO | An experimental study of aerodynamic characteristics of longitudinally truncated cylinders and cone-cylinders(reentry effects on sounding rockets) | |
WYKES et al. | XB-70 aerodynamic, geometric, mass, and symmetric structural mode data(Analysis of mass, structural, and aerodynamic data for XB-7 aircraft at three flight conditions) | |
AILMAN | Turbulent-boundary-layer excitation and response thereto for a high-performance conical vehicle(reentry) | |
Blanchard | Drag and Longitudinal Trim at Low Lift of the North American YF-100A Airplane at Mach Numbers from 0.76 to 1.77 as Determined from the Flight Test of a 0.11-Scale Rocket Model | |
Golub et al. | In-flight measurement of rotor blade airloads, bending moments, and motions, together with rotor shaft loads and fuselage vibration, on a tandem rotor helicopter. Volume 1- Instrumentation and in-flight recording system(Instrumentation and recording system for aerodynamic loads and load effects on rotor and fuselage of flying tandem helicopter) | |
Howard et al. | Tumbling susceptibility of a tailless unmanned air vehicle | |
Flomenhoft | Some early cases of servo-elastic interactions | |
BROADHURST | Installation and validation of an airborne data acquisition system aboard a Cessna 310 H use as a flying laboratory[M. S. Thesis] | |
MOORE | Aeroservoelastic stability analysis of an airplane with a control augmentation system[Ph. D. Thesis] | |
Gill et al. | The Hunter fly-by-wire experiment: Recent experience and future implications |