Author: A. J. Fairbanks
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
Book Description
Pressure Distribution Tests on PW-9 Wing Models Showing Effects of Biplane Interference
Pressure Distribution Tests on P-9 Wing Models Showing Effects of Biplane Interference
Author: A. J. Fairbanks
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 0
Book Description
Pressure Distribution Over a Rectangular Monoplane Wing Model Up to 90 ̊angle of Attack
Author: A. F. Zahm
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 90
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 90
Book Description
The N.A.C.A. Photographic Apparatus for Studying Fuel Sprays from Oil Engine Injection Valves and Test Results from Several Researches
Author: A. J. Fairbanks
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 172
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 172
Book Description
The Variation in Engine Power with Altitude Determined from Measurements in Flight with a Hub Dynamometer
Author: Chester W. Hicks
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 218
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 218
Book Description
Flight-test Data on the Static Fore-and-aft Stability of Various German Airplanes
Author: Walter Hübner
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 668
Book Description
The static longitudinal stability of an airplane with locked elevator is usually determined by analysis and model tests. The present report proposes to supply the results of such measurements. The method consisted of recording the dynamic pressure versus elevator displacement at different center-of-gravity positions in unaccelerated flight.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 668
Book Description
The static longitudinal stability of an airplane with locked elevator is usually determined by analysis and model tests. The present report proposes to supply the results of such measurements. The method consisted of recording the dynamic pressure versus elevator displacement at different center-of-gravity positions in unaccelerated flight.
Bibliography of Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 228
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 228
Book Description
Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 16
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 16
Book Description
Report
Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 660
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 660
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.