Related Books

Static Force Tests of a Model of a Twin-jet Fighter Airplane for Angles of Attack from -100 to 1100 and Sideslip Angles from -400 to 400
Language: en
Pages: 100

Static Force Tests of a Model of a Twin-jet Fighter Airplane for Angles of Attack from -100 to 1100 and Sideslip Angles from -400 to 400

Authors: Ernie L. Anglin
Categories: Airplanes
Type: BOOK - Published: 1971 - Publisher:

DOWNLOAD EBOOK

Static force tests of model of twin jet fighter aircraft at various angles of attack and sideslip angles to obtain data for theoretical spin studies.
Static Force Tests of a Model of a Twin-jet Fighter Airplane for Angles of Attack from -100 to 1100 and Sideslip Angles from -400 to 400
Language: en
Pages: 0

Static Force Tests of a Model of a Twin-jet Fighter Airplane for Angles of Attack from -100 to 1100 and Sideslip Angles from -400 to 400

Authors: Ernie L. Anglin
Categories: Airplanes
Type: BOOK - Published: 1971 - Publisher:

DOWNLOAD EBOOK

Static Force Tests of a Model of a Twin-jet Fighter Airplane for Angles of Attack from -10° to 110° and Sideslip Angles from -40° to 40°
Language: en
Pages: 89

Static Force Tests of a Model of a Twin-jet Fighter Airplane for Angles of Attack from -10° to 110° and Sideslip Angles from -40° to 40°

Authors: Ernie L. Anglin
Categories: Airplanes
Type: BOOK - Published: 1971 - Publisher:

DOWNLOAD EBOOK

Static force tests of model of twin jet fighter aircraft at various angles of attack and sideslip angles to obtain data for theoretical spin studies.
Static Force Tests of a Model of a Twin-jet Fighter Airplane for Angles of Attack from -10 Degrees to 110 Degrees and Sideslip Angles from -40 Degrees to 40 Degrees
Language: en
Pages: 89

Static Force Tests of a Model of a Twin-jet Fighter Airplane for Angles of Attack from -10 Degrees to 110 Degrees and Sideslip Angles from -40 Degrees to 40 Degrees

Authors: Ernie L. Anglin
Categories:
Type: BOOK - Published: 1971 - Publisher:

DOWNLOAD EBOOK

Dynamic Stability Derivatives of a Twin-jet Fighter Model for Angles of Attack from -10 ̊to 110 ̊
Language: en
Pages: 44

Dynamic Stability Derivatives of a Twin-jet Fighter Model for Angles of Attack from -10 ̊to 110 ̊

Authors: Sue B. Grafton
Categories: Airplanes
Type: BOOK - Published: 1971 - Publisher:

DOWNLOAD EBOOK

A low-speed investigation was conducted to determine the dynamic stability derivatives in pitch, roll, and yaw over an angle-of-attack range of -10 [degree] to