Author: Richard K. Grief
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 112
Book Description
Large-scale Wind-tunnel Tests of a Circulation Plan-form Aircraft with a Peripheral Jet for Lift, Thrust, and Control
Author: Richard K. Grief
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 112
Book Description
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 112
Book Description
Large-scale Wind-tunnel Tests of a Circulation Plan-form Aircraft with a Peripheral Jet for Lift, Thrust, and Control
Author: Richard K. Grief
Publisher:
ISBN:
Category :
Languages : en
Pages : 97
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 97
Book Description
Results of Full-scale Wind Tunnel Tests on the H.126 Jet Flap Aircraft
Author: Anthony M. Cook
Publisher:
ISBN:
Category : Jet flaps (Airplanes)
Languages : en
Pages : 66
Book Description
Publisher:
ISBN:
Category : Jet flaps (Airplanes)
Languages : en
Pages : 66
Book Description
Large-scale Wind-tunnel Investigation of a Model with an External Jet-augmented Flap
Author: Jerry V. Kirk
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
VTOL/STOL Aircraft
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 344
Book Description
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 344
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 260
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 260
Book Description
FULL SCALE WIND TUNNEL TEST REPORT.
Author: GENERAL ELECTRIC CO CINCINNATI OHIO ADVANCED TECHNOLOGY AND DEMONSTRATOR PROGRAMS Dept
Publisher:
ISBN:
Category :
Languages : en
Pages : 303
Book Description
The test program included aerodynamic, thermodynamic and mechanical evaluation of the complete flight type aircraft system at flight speeds equivalent to hover up through 100 knots in both the conventional and fan power modes of flight. The report summarizes the more important aerodynamic performance obtained during the test program. The data are presented graphically in coefficient form to provide a consistent basis of comparison. The aerodynamic results obtained during these tests may be summarized by saying that the aircraft, as designed and tested, has adequate control power, lift, horizontal thrust and static stability to permit safe transitional flight between a hover lift-off and conversion to the jet mode of flight. The results of this wind tunnel test program have proven to be a valuable asset during conduct of the flight test program. Using these data, predictions of aircraft performance have been verified by actual measured flight data. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 303
Book Description
The test program included aerodynamic, thermodynamic and mechanical evaluation of the complete flight type aircraft system at flight speeds equivalent to hover up through 100 knots in both the conventional and fan power modes of flight. The report summarizes the more important aerodynamic performance obtained during the test program. The data are presented graphically in coefficient form to provide a consistent basis of comparison. The aerodynamic results obtained during these tests may be summarized by saying that the aircraft, as designed and tested, has adequate control power, lift, horizontal thrust and static stability to permit safe transitional flight between a hover lift-off and conversion to the jet mode of flight. The results of this wind tunnel test program have proven to be a valuable asset during conduct of the flight test program. Using these data, predictions of aircraft performance have been verified by actual measured flight data. (Author).
Wind Tunnel Test Techniques
Author: Colin Britcher
Publisher: Academic Press
ISBN: 0128181001
Category : Technology & Engineering
Languages : en
Pages : 672
Book Description
Wind Tunnel Test Techniques: Design and Use at Low and High Speeds with Statistical Engineering Applications provides an up-to-date treatment of the topic. Beginning with a brief history of wind tunnels and its types and uses, the book goes on to cover subsonic, supersonic and hypersonic wind tunnel design and construction, calibration, boundary corrections, flow quality assessment, pressure surveys, and dynamic testing. It also focuses on wind tunnel facilities, making it useful for both the designer and operator. Engineers and graduate students in aerospace, automotive and similar programs will find this book useful in their work with experimental aerodynamics, gas dynamics, facility design and performance. Deals with a broad range of flow speeds in wind tunnels, from low speed to high speed Provides a discussion of similarity laws as well as material on statistical analysis Includes coverage on facility-to-facility and facility-to-CFD correlation Presents advanced topics such as cryogenic wind tunnels, ground simulation in automotive testing, and propulsion testing
Publisher: Academic Press
ISBN: 0128181001
Category : Technology & Engineering
Languages : en
Pages : 672
Book Description
Wind Tunnel Test Techniques: Design and Use at Low and High Speeds with Statistical Engineering Applications provides an up-to-date treatment of the topic. Beginning with a brief history of wind tunnels and its types and uses, the book goes on to cover subsonic, supersonic and hypersonic wind tunnel design and construction, calibration, boundary corrections, flow quality assessment, pressure surveys, and dynamic testing. It also focuses on wind tunnel facilities, making it useful for both the designer and operator. Engineers and graduate students in aerospace, automotive and similar programs will find this book useful in their work with experimental aerodynamics, gas dynamics, facility design and performance. Deals with a broad range of flow speeds in wind tunnels, from low speed to high speed Provides a discussion of similarity laws as well as material on statistical analysis Includes coverage on facility-to-facility and facility-to-CFD correlation Presents advanced topics such as cryogenic wind tunnels, ground simulation in automotive testing, and propulsion testing
Full-scale Wind-tunnel Tests of a Swept-wing Airplane with a Cascade-type Thrust Reverser
Author: Mark W. Kelly
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description