This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
A Look at V/STOL for Business Aircraft
Annotation ability available
Sector:
Language:
English
Abstract
This paper addresses the three questions: “Is V/STOL capability economically viable for business aircraft, and if so, how does the viability depend on the aircraft concept?”; “How is a V/STOL concept chosen to match a given mission, and what are some of the promising V/STOL concepts for future business aircraft?”; and “What unique operational requirements are likely to be imposed on users of future V/STOL business aircraft?”
A cost-benefit analysis is presented which indicates that a VTOL business aircraft would be more viable economically than a contemporary turbine-powered business aircraft. The combinations of traveler's time value and trip distance for which each aircraft dominates is shown. A discussion is presented on the significance of disc loading as it relates to V/STOL concept application. Preliminary design configuration studies for three different business-aircraft-sized V/STOLs, using three concepts covering a range of disc loading, are presented as examples. A discussion of operational aspects of interest to future users of V/STOL business aircraft by a NASA test pilot with VTOL research aircraft experience is centered around the requirements for routine IFR terminal area operations.
Recommended Content
Book | Fly-By-Wire |
Technical Paper | A Perspective on the First Century of Vertical Flight |
Authors
Topic
Citation
Feistel, T., Stewart, E., Gerdes, R., and Smith, K., "A Look at V/STOL for Business Aircraft," SAE Technical Paper 720334, 1972, https://doi.org/10.4271/720334.Also In
References
- “NASA Conference on V/STOL Aircraft, Langley Field, 1960-A Compilation of the Papers Presented.” NASA November 1960
- “Conference on V/STOL and STOL Aircraft.” NASA SP-116 1966
- “Move to the Cities.” Flight Magazine January 1970
- Harned M. “Thoughts on Business Aircraft in the 1980s.” Professional Pilot February 1970
- Siekman P. “The Plane That Could Teach An Industry to Fly.” Fortune April 1971
- Smith, K. R. Jr. Belina F. W. Forthcoming NASA CR The Aerospace Corp. Ames Research Center
- Kahn J. T. “V/STOL Airline System Simulation.” AIAA Paper No. 67-841 1967
- “Recommendations for Northeast Corridor Transportation.” 1-3 U.S. Dept. of Transportation May 1971
- Drake H. M. Kenyon G. C. Galloway T. L. “Mission Analysis for General Aviation in the 1970s.” AIAA Paper No. 69-818 1969
- Kenyon G. C. Galloway T. L. Drake H. M. “An Economic Analysis of Future Short-Haul Transportation.” 1971
- “Some Thoughts About the Merits of Owning a Business Jet.” Gates Learjet Contrails 4 1 May 1971 4 5
- Wick B. H. Kuhn R. A. “Turbofan STOL Research at NASA.” Astronautics and Aeronautics 9 5 May 1971
- Middlebrooks J. E. Tinney H. C. Whittley D. C. “The Evolutionary Development and Current Status of the Augmentor Wing Concept.” Paper 700812 National Aeronautics and Space Engineering and Manufacturing Meeting Los Angeles October 1970
- Loftin, L. K. Jr. McKinney, M. D. Jr. “NASA Aerodynamic Research Applicable to Business Aircraft.” Paper 710378 SAE National Business Aircraft Meeting Wichita, Kans. March 1971
- Chatham G. N. “Toward Aircraft of the 1980s.” Astronautics & Aeronautics July 1968 26
- Rosen G. “Filling the Propulsion Gaps.” Space/Aeronautics May 1970 31
- Hafner R. “The Domain of the Convertible Rotor.” AIAA Preprint No. 63-483 1963
- Hurkamp C. H. Johnston W. M. Wilson J. H. “Technology Assessment of Advanced General Aviation Aircraft.” 1971
- DeTore J. A. “Lift/Propulsion System Size-Selection Considerations for Stoppable Rotor VTOL Aircraft.” Air Force V/STOL Tech. and Planning Conf. Las Vegas, Nev. Sept. 23-25 1969
- Wernicke K. G. Edenborough H. K. “Full-Scale Proprotor Development.” AHS Preprint No. 501 May 1971
- Quigley H. C. Koenig D. G. “The Effect of Blade Flapping on the Dynamic Stability of A Tilting-Rotor Convertiplane.” 1961
- Kelley H. L. Reeder J. P. Champine R. A. “Summary of a Flight-Test Evaluation of the CL-84 Tilt-Wing V/STOL Aircraft.” 1970
- Worobel R. Mayo M. G. “Advanced General Aviation Propeller Study.” 1971
- Hickey D. H. Cook W. L. “Aerodynamics of V/STOL Aircraft Powered by Lift Fans.” 1967
- Kirk J. V. Hall L. P. Hodder B. K. “Aerodynamics of Lift Fan V/STOL Aircraft.” 1971
- Finnestead R. Ferrell K. Welter W. Anderson W. “Engineering Flight Research Evaluation of the XV-5A Lift Fan Aircraft.” USAAVNTA Project No. 62-72, U.S. Army Aviation Test Activity Edwards AFB Calif. August 1966
- Gerdes R. M. Hynes C. S. “Factors Affecting Handling Qualities of a Lift-Fan Aircraft During Steep Terminal Area Approaches.” AHS Preprint No. 544, 27th Annual National V/STOL Forum Washington, D.C. May 1971
- “V/STOL Handling I-Criteria and Discussion.” 1970
- Novak L. R. “A Low Risk Approach to Development of a Quiet V/STOL Transport Aircraft.” AIAA Paper No. 70-1409 7th Annual Meeting of AIAA Houston, Texas Oct. 19-22 1970
- Bland A. M. “Fan Propulsion System Influence on VTOL Transport Design.” 7th Propulsion Joint Specialist Conf. at the AIAA and SAE Salt Lake City, Utah June 14-18 1971
- Person L. Morello S. A. Holzhauser C. A. Gerdes R. M. “Operational Aspects of V/STOL Instrument Approaches.” NASA SP 270 1971 233
- Greif R. K. Fry E. B. Gerdes R. M. Gossett T. D. “VTOL Control System Studies on a 6 Degree-of-Freedom Motion Simulator.” ICAS paper No. 66-9, 5th Congress of the International Council of the Aeronautical Sciences London, England September 1966
- Innis R. C. Holzhauser C. A. Quigley H. C. “Airworthiness Considerations for STOL Aircraft.” 1970
- Kelley J. R. Niessen F. R. Sommer R. W. “Evaluation of a VTOL Flight-Director Concept During Constant-Speed Instrument Approaches.” 1970
- Gracey W. Sommer R. W. Tibbs D. F. “Evaluation of a Moving Map Instrument Display in Landing Approaches with a Helicopter.” 1967