Flight Measurement Of The Stability Characteristics Of The Douglas D 558 1 Airplane Buaero No 37971 In Sideslips

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Flight Measurement of the Stability Characteristics of the Douglas D-558-1 Airplane (Buaero No. 37971) in Sideslips

Flight Measurement of the Stability Characteristics of the Douglas D-558-1 Airplane (Buaero No. 37971) in Sideslips
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Total Pages : 28
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ISBN-10 : UOM:39015086464354
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Book Synopsis Flight Measurement of the Stability Characteristics of the Douglas D-558-1 Airplane (Buaero No. 37971) in Sideslips by : Walter C. Williams

Download or read book Flight Measurement of the Stability Characteristics of the Douglas D-558-1 Airplane (Buaero No. 37971) in Sideslips written by Walter C. Williams and published by . This book was released on 1949 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Flight Measurement of the Stability Characteristics of the Douglas D-558-1 Airplane (Buaero No. 37971) in Sideslips Related Books

Flight Measurement of the Stability Characteristics of the Douglas D-558-1 Airplane (Buaero No. 37971) in Sideslips
Language: en
Pages: 28
Authors: Walter C. Williams
Categories: Douglas airplanes
Type: BOOK - Published: 1949 - Publisher:

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Measured Characteristics of the Douglas D-558-1 Airplane (BUAERO NO. 37971) in Two Landings
Language: en
Pages: 8
Authors: Hubert M. Drake
Categories: Airplanes
Type: BOOK - Published: 1949 - Publisher:

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Records were obtained of two landings of the Douglas D-558-1 airplane during the stability and control investigation. These two records show that the maximum no
Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane
Language: en
Pages:
Authors: S. A. Sjoberg
Categories:
Type: BOOK - Published: 1950 - Publisher:

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Stability Results Obtained with Douglas D-558-1 Airplane (BuAero No. 37971) in Flight Up to a Mach Number of 0.89
Language: en
Pages: 16
Measurement of the Dynamic Lateral Stability of the Douglas D-558-1 Airplane (BUAERO No. 37971) in Rudder Kicks at a Mach Number of 0.72
Language: en
Pages: 10
Authors: Hubert M. Drake
Categories: Airplanes
Type: BOOK - Published: 1949 - Publisher:

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In the course of a stability and control investigation of the D-558-1 airplane, rudder kicks were made at a Mach number of 0.72 at a pressure altitude of 8500 f