In-flight Temperature Measurements

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Publisher :
ISBN 13 :
Total Pages : 184 pages
Book Rating : 4.:/5 (318 download)

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Book Synopsis In-flight Temperature Measurements by : Fritz Trenkle

Download or read book In-flight Temperature Measurements written by Fritz Trenkle and published by . This book was released on 1973 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Advanced In-Flight Measurement Techniques

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Publisher : Springer Science & Business Media
ISBN 13 : 364234738X
Total Pages : 347 pages
Book Rating : 4.6/5 (423 download)

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Book Synopsis Advanced In-Flight Measurement Techniques by : Fritz Boden

Download or read book Advanced In-Flight Measurement Techniques written by Fritz Boden and published by Springer Science & Business Media. This book was released on 2013-02-13 with total page 347 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book presents a synopsis of the main results achieved during the 3 year EU-project "Advanced Inflight Measurement Techniques (AIM)" which applied advanced image based measurement techniques to industrial flight testing. The book is intended to be not only an overview on the AIM activities but also a guide on the application of advanced optical measurement techniques for future flight testing. Furthermore it is a useful guide for engineers in the field of experimental methods and flight testing who face the challenge of a future requirement for the development of highly accurate non-intrusive in-flight measurement techniques.

Flight Measurements of Airplane Structural Temperatures at Supersonic Speeds

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Flight Measurements of Airplane Structural Temperatures at Supersonic Speeds by : Richard D. Banner

Download or read book Flight Measurements of Airplane Structural Temperatures at Supersonic Speeds written by Richard D. Banner and published by . This book was released on 1957 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: Skin and structural temperatures have been obtained on the X-1B and X-1E research airplanes under transient aerodynamic heating conditions at speeds up to Mach numbers near 2.0. Extensive temperature measurements were obtained throughout the X-1B airplane, and temperature distributions are shown on the nose cone, the wing, and the vertical tail. Temperatures for the X-1E wing leading edge and internal wing structure were compared with similar data for the X-1B. No critical skin and structural temperatures were obtained on the two airplanes over the range of these tests. Simplified calculations of the skin temperatures in the laminar-flow regions of the nose cone and the leading edges agreed favorably with the general trends in the measured data. The flat-plate skin-temperature calculations in the turbulent-flow regions agreed favorably with the measured data on the nose cone and at the midsemispan station of the wing but overestimated the vertical-tail skin temperatures and also the upper wing skin temperature near the wing tip. The relatively low values of the upper skin temperatures that were measured at the wing tip were believed to be caused by separated-flow effects in this region.

Free-flight Skin-temperature and Surface-pressure Measurements on a Highly Polished Nose Having a 1000 Total-angle Cone and a 100 Half-angle Conical Flare Section Up to a Mach Number of 4.08

Download Free-flight Skin-temperature and Surface-pressure Measurements on a Highly Polished Nose Having a 1000 Total-angle Cone and a 100 Half-angle Conical Flare Section Up to a Mach Number of 4.08 PDF Online Free

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Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Free-flight Skin-temperature and Surface-pressure Measurements on a Highly Polished Nose Having a 1000 Total-angle Cone and a 100 Half-angle Conical Flare Section Up to a Mach Number of 4.08 by : Bernard Rashis

Download or read book Free-flight Skin-temperature and Surface-pressure Measurements on a Highly Polished Nose Having a 1000 Total-angle Cone and a 100 Half-angle Conical Flare Section Up to a Mach Number of 4.08 written by Bernard Rashis and published by . This book was released on 1961 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Measurements of Aerodynamic Heating Obtained During Demonstration Flight Tests of the Douglas D-558-II Airplane

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Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Measurements of Aerodynamic Heating Obtained During Demonstration Flight Tests of the Douglas D-558-II Airplane by : Ira P. Jones

Download or read book Measurements of Aerodynamic Heating Obtained During Demonstration Flight Tests of the Douglas D-558-II Airplane written by Ira P. Jones and published by . This book was released on 1952 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Airliner Cabin Environment and the Health of Passengers and Crew

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Publisher : National Academies Press
ISBN 13 : 0309082897
Total Pages : 345 pages
Book Rating : 4.3/5 (9 download)

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Book Synopsis The Airliner Cabin Environment and the Health of Passengers and Crew by : National Research Council

Download or read book The Airliner Cabin Environment and the Health of Passengers and Crew written by National Research Council and published by National Academies Press. This book was released on 2002-02-03 with total page 345 pages. Available in PDF, EPUB and Kindle. Book excerpt: Although poor air quality is probably not the hazard that is foremost in peoples' minds as they board planes, it has been a concern for years. Passengers have complained about dry eyes, sore throat, dizziness, headaches, and other symptoms. Flight attendants have repeatedly raised questions about the safety of the air that they breathe. The Airliner Cabin Environment and the Health of Passengers and Crew examines in detail the aircraft environmental control systems, the sources of chemical and biological contaminants in aircraft cabins, and the toxicity and health effects associated with these contaminants. The book provides some recommendations for potential approaches for improving cabin air quality and a surveillance and research program.

Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration

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Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration by : Charles B. Rumsey

Download or read book Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration written by Charles B. Rumsey and published by . This book was released on 1955 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle conical nose of a rocket-propelled model at flight Mach numbers of 1.4 to 3.9. The corresponding values of local Reynolds number varied from 18,000,000 to 46,000,000 and the ratio of skin temperature to local static temperature varied from 1.2 to 2.4. The experimental data, reduced to Stanton number, were in fair agreement with values predicted by Van Driest's theory for heat transfer on a cone with turbulent flow from the nose tip.

Accuracy of Airspeed Measurements and Flight Calibration Procedures

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Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Accuracy of Airspeed Measurements and Flight Calibration Procedures by : Wilber B. Huston

Download or read book Accuracy of Airspeed Measurements and Flight Calibration Procedures written by Wilber B. Huston and published by . This book was released on 1948 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report reviews in detal the sources of error that may enter into the measurement of airspeed by pitot-static methods. Methods of flight calibration of airspeed installations are given. Special attention is given to the problem of accurate measurement of Mach number, air temperature, and true airspeed during high-speed maneuvers. This report also contains an extensive bibliography.

The Variation in Engine Power with Altitude Determined from Measurements in Flight with a Hub Dynamometer

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Publisher :
ISBN 13 :
Total Pages : 218 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis The Variation in Engine Power with Altitude Determined from Measurements in Flight with a Hub Dynamometer by : Chester W. Hicks

Download or read book The Variation in Engine Power with Altitude Determined from Measurements in Flight with a Hub Dynamometer written by Chester W. Hicks and published by . This book was released on 1928 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Instrumentation Requirements for a Flight Reentry Heating Experiment at Interplanetary Return Velocity

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Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Instrumentation Requirements for a Flight Reentry Heating Experiment at Interplanetary Return Velocity by : Elden S. Cornette

Download or read book Instrumentation Requirements for a Flight Reentry Heating Experiment at Interplanetary Return Velocity written by Elden S. Cornette and published by . This book was released on 1971 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Telemetry Theory and Methods in Flight Test

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Publisher : Springer Nature
ISBN 13 : 9813347376
Total Pages : 475 pages
Book Rating : 4.8/5 (133 download)

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Book Synopsis Telemetry Theory and Methods in Flight Test by : Tingwu Yang

Download or read book Telemetry Theory and Methods in Flight Test written by Tingwu Yang and published by Springer Nature. This book was released on 2021-03-25 with total page 475 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book describes systematically telemetry theory and methods for aircraft in flight test. Test targets of telemetry in flight test include airplanes, helicopters, unmanned aerial vehicles, aerostatics, carrier-based aircraft, airborne equipment (systems), weapon systems, (powered) aircraft scale models, aircraft external stores (e.g., nacelle, auxiliary tanks), and ejection seats and so on. The book collects the author's telemetry research work and presents methods that have been verified in real-world tests. The book has eight chapters: the first three discuss the theoretical basis of telemetry, while the other five focus on the methods used in flight tests.Unlike other professional textbooks, this book describes the practical telemetry theory and combines theory and engineering practice to offer a comprehensive and systematic overview of telemetry in flight test for readers.

Flight-test Results from Two Total Temperature Probes for Air-data Measurements Up to 2014 ̊K (3625 ̊R)

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Publisher :
ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Flight-test Results from Two Total Temperature Probes for Air-data Measurements Up to 2014 ̊K (3625 ̊R) by : Jack Nugent

Download or read book Flight-test Results from Two Total Temperature Probes for Air-data Measurements Up to 2014 ̊K (3625 ̊R) written by Jack Nugent and published by . This book was released on 1972 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental temperature probe package containing a fluidic oscillator temperature probe and a shielded thermocouple temperature probe was tested during several X-15 flights. The X-15 flights provided greatly varying test conditions, including a wide range of rapidly changing total temperatures and Mach numbers which extended from subsonic to hypersonic speeds. Within restricted ranges of free-stream Mach number, free-stream unit weight flow, and local stagnation pressure, both probes yielded ramp outputs of temperature parallel to ramp inputs of free-stream total temperature. Within these ranges both probes were used to determine total temperature in the Mach 6 temperature environment. Because ambient temperature was known, both probes were used to estimate velocity and Mach number.

Measurements of Sea Surface Temperature on the Eastern Pacific Continental Shelf Using Airborne Infrared Radiometry, August 1963-July 1968

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Publisher :
ISBN 13 :
Total Pages : 240 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Measurements of Sea Surface Temperature on the Eastern Pacific Continental Shelf Using Airborne Infrared Radiometry, August 1963-July 1968 by : James L. Squire

Download or read book Measurements of Sea Surface Temperature on the Eastern Pacific Continental Shelf Using Airborne Infrared Radiometry, August 1963-July 1968 written by James L. Squire and published by . This book was released on 1971 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Recent Flight-test Results of Optical Airdata Techniques

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Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Recent Flight-test Results of Optical Airdata Techniques by : Rodney K. Bogue

Download or read book Recent Flight-test Results of Optical Airdata Techniques written by Rodney K. Bogue and published by . This book was released on 1993 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 290 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 290 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Introduction to Aerospace Engineering with a Flight Test Perspective

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Publisher : John Wiley & Sons
ISBN 13 : 1118953363
Total Pages : 931 pages
Book Rating : 4.1/5 (189 download)

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Book Synopsis Introduction to Aerospace Engineering with a Flight Test Perspective by : Stephen Corda

Download or read book Introduction to Aerospace Engineering with a Flight Test Perspective written by Stephen Corda and published by John Wiley & Sons. This book was released on 2017-03-20 with total page 931 pages. Available in PDF, EPUB and Kindle. Book excerpt: Comprehensive textbook which introduces the fundamentals of aerospace engineering with a flight test perspective Introduction to Aerospace Engineering with a Flight Test Perspective is an introductory level text in aerospace engineering with a unique flight test perspective. Flight test, where dreams of aircraft and space vehicles actually take to the sky, is the bottom line in the application of aerospace engineering theories and principles. Designing and flying the real machines are often the reasons that these theories and principles were developed. This book provides a solid foundation in many of the fundamentals of aerospace engineering, while illuminating many aspects of real-world flight. Fundamental aerospace engineering subjects that are covered include aerodynamics, propulsion, performance, and stability and control. Key features: Covers aerodynamics, propulsion, performance, and stability and control. Includes self-contained sections on ground and flight test techniques. Includes worked example problems and homework problems. Suitable for introductory courses on Aerospace Engineering. Excellent resource for courses on flight testing. Introduction to Aerospace Engineering with a Flight Test Perspective is essential reading for undergraduate and graduate students in aerospace engineering, as well as practitioners in industry. It is an exciting and illuminating read for the aviation enthusiast seeking deeper understanding of flying machines and flight test.

A Study of the Accuracy of a Flight-heating Simulation and Its Effect on Load Measurement

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Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Study of the Accuracy of a Flight-heating Simulation and Its Effect on Load Measurement by : Roger A. Fields

Download or read book A Study of the Accuracy of a Flight-heating Simulation and Its Effect on Load Measurement written by Roger A. Fields and published by . This book was released on 1970 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: