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Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3

Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3 PDF Author: Hill, Jr. (William A.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 102

Book Description


Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3

Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3 PDF Author: Hill, Jr. (William A.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 102

Book Description


Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3

Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 96

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1714

Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572

Book Description


Investigation, at Inlet Locations, of Fuselage Flow Fields at Transonic and Supersonic Speeds

Investigation, at Inlet Locations, of Fuselage Flow Fields at Transonic and Supersonic Speeds PDF Author: Lyndell S. King
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 132

Book Description
Wind tunnel tests were conducted to determine the flow distribution about fuselage configurations at transonic and supersonic speeds and at angles of attack up to 20 degrees. The models tested were approximately one-twelfth scale and consisted of a main fuselage forebody member and several attachable components. The components were mounted in several combinations to represent different possible configurations for tactical aircraft. Flow distribution surveys were conducted at two inlet locations ahead of and under the wing to assess the effects of forebody geometry for the conditions indicated. The data indicate the influence of the canopy, nose droop, and fuselage shape on flow angularities in the forward survey plane.

NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440

Book Description


A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
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Category : Aeronautics
Languages : en
Pages : 818

Book Description


Determination of Captive Flight Loads and Separation Trajectories of Airborne Stores

Determination of Captive Flight Loads and Separation Trajectories of Airborne Stores PDF Author: Dale E. Knutsen
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 72

Book Description


Measurements of Flow Properties in the Vicinity of Three Wing-fuselage Combinations at Mach Numbers of 1.61 and 2.01

Measurements of Flow Properties in the Vicinity of Three Wing-fuselage Combinations at Mach Numbers of 1.61 and 2.01 PDF Author: Harry W. Carlson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 78

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 688

Book Description