SPLETTSTOESSER et al., 1982 - Google Patents
Helicopter noise certification and sensitivity studies along the procedural lines of the new ICAO Annex 16/Chapter 8 regulationsSPLETTSTOESSER et al., 1982
- Document ID
- 7321368948374752895
- Author
- SPLETTSTOESSER W
- HELLER H
- Kloeppel V
- Publication year
- Publication venue
- Association Aeronautique et Astronautique de France, European Rotorcraft Forum, 8 th, Aix-en-Provence, France
External Links
- 230000035945 sensitivity 0 title abstract description 6
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/008—Rotors tracking or balancing devices
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1530245A (en) | Helicopter apparatus | |
SPLETTSTOESSER et al. | Helicopter noise certification and sensitivity studies along the procedural lines of the new ICAO Annex 16/Chapter 8 regulations | |
Hunter et al. | An Analysis of VG and VGH Operational Data From a Twin-Engine Turboprop Transport Airplane | |
Loschke et al. | Flight Evaluations of the Effect of Advanced Control Systems and Displays on the Handling Qualities of a General Aviation Airplane | |
POMEROY et al. | C-141 A pitot-static system calibration tests | |
FOX | Helicopter accident trends | |
NATTER | Take-off and landing problems of ship based RPVs | |
Kranenburg et al. | Operational application of the STALINS method for measuring take-off and landing trajectories | |
STRONG et al. | Noise levels in the CH-113 A and CUH-IN helicopter | |
PHILLIPS | Altitude response of several airplanes during landing approach(including space shuttle) | |
Taghizad et al. | Evaluation of helicopter handling qualities improvements during a steep approach using new piloting modes | |
Matranga et al. | Flight-determined Static Lateral Stability and Control Characteristics of a Swept-wing Fighter Airplane to a Mach Number of 1.39 | |
Young | Development of the vortex ring wake model and its influence on the prediction of rotor loads | |
LAWTON | General aviation icing flight test | |
Baker | Some Measurements of Buffeting Encountered by Douglas D-558-II Research Airplane in the Mach Number Range from 0.5 to 0.95 | |
WARNIX et al. | YC-15 interior noise measurements. Technical discussion[Final Report, 8 May- 8 Dec. 1976] | |
TEPER et al. | Preliminary Candidate Advanced Avionics System(PCAAS)(reduction in single pilot workload during instrument flight rules flight)[Final Report] | |
HUTCHINS | Navy vehicle design and construction: Measurement of triaxial vibration at significant human interface points on the CH-47 C and SH-3 A helicopters(Measurement of vibration levels in CH-47 helicopter at pilot seat, control stick, rudder pedals, instrument panel, and human interface points)[Final Report] | |
BONAFE | How to fly windshear using the fly-by-wire concept | |
PICASSO | Airworthiness and Flight Characteristics(AFC) test of YAH-64 advanced attack helicopter, Prototype Qualification Test-Government(PQT-G), part 3 and Production Validation Test-Government(PVT-G) for handbook verification[Final Report, 12 May- 19 Aug. 1982] | |
WILKINS | In the beginning- Ab initio training for tiltrotor crews | |
Faulkner et al. | Handling qualities and flight performance- Implication of the operational envelope | |
TEIN | Development and certification of the BK 117 multipurpose helicopter | |
LAMBERT | Flying the CF-18 Hornet | |
WARREN | Safety criteria for fail-operational autoland systems and their application(for civil aviation) |