CAL/TRECOM SYMPOSIUM PROCEEDINGS VOL 2. DYNAMIC LOAD PROBLEMS ASSOCIATED WITH HELICOPTERS AND V/STOL AIRCRAFT, JUNE 26-28, 1963, BUFFALO, N.Y
Abstract
Contents: A Review of the Structural Dynamic Characteristics of the XC-142A Aircraft; Propeller Whirl Flutter Considerations for V/STOL Aircraft; High-Speed Shafting for Power Transmission in Aircraft; Dynamic Torsional Problems in VTOL Drive Trains with Universal Joints; Recent Work at the Royal Aircraft Establishment on Helicopter Dynamic Loads, with Particular Reference to High Blade Incidence Problems; Some Results from the Army Low Altitude, High- Speed Flight Program (Man-Machine); Human Factor Problems Associated with Low Altitude High-Speed (LAHS) Flight: Effect of Gust Alleviation System on Dynamic Airloads; and An Analytical Investigation of Aircraft Loads Induced by Rough Terrain Landings.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 28, 1963
- Accession Number
- AD0819971