Inventor profile of:

Alan E. Arslan

City:

Santa Clarita, California

Country:

United States

Published Applications:

12

Last publication date:

2007-11-15

Top Assignees for applications by Alan E. Arslan

The entities that hold a legal rights for patent applications filed by inventor Arslan Alan E.:

Recent patent applications by Arslan Alan E.

Alan E. Arslan from Santa Clarita, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2007-11-15
US20070262207A1
Performing operations; transporting

Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance

#2 | 2006-10-26
US20060237580A1
Performing operations; transporting

Canard position and dihedral for boom reduction and pitch/directional control

#3 | 2006-03-16
US20060058985A1
Physics

Adjoint-based design variable adaptation

#4 | 2005-10-13
US20050224640A1
Performing operations; transporting

Methods for incorporating area ruled surfaces in a supersonic aircraft

#5 | 2005-06-09
US20050121555A1
Performing operations; transporting

Mach weighted area ruling for supersonic vehicles

#6 | 2005-06-02
US20050116108A1
Performing operations; transporting

Methods for configuring aircraft to meet performance goals and shock wave disturbance constraints

#7 | 2005-06-02
US20050116107A1
Performing operations; transporting

Area ruling for vertical stabilizers

#8 | 2005-05-19
US20050103929A1
Performing operations; transporting

Supersonic aircraft with channel relief control

#9 | 2005-03-31
US20050067526A1
Performing operations; transporting

Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction

#10 | 2005-03-31
US20050067525A1
Performing operations; transporting

Aircraft thickness/camber control device for low sonic boom

#11 | 2005-03-03
US20050045764A1
Performing operations; transporting

Canard position and dihedral for boom reduction and pitch/directional control

#12 | 2005-02-15
US10713515
-

Nacelle integration with reflexed wing for sonic boom reduction

InventorID:

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