NASA / TM X-519
Robinson,Ross B
EFFECT OF VERTICLE-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS / .- Nasa, Washington, D.C., 1961 .- 17 .
Bound With Nasa Tm X-507-18,522-81, Lack No.509-13,515-17,519-21,523-29,531-39,541-46,548-65,567-68,572-80
Author Added Entry:
Spearman,M Leroy;
Copy Details:
Acc. No.: TR14307, Full Call No.: NASA TM X-519, Item type: Technical Report , Location: General Stacks,
------------------------- --------------------- ------ --------- ------- ------- --------- --------
Robinson,Ross B
EFFECT OF VERTICLE-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS / .- Nasa, Washington, D.C., 1961 .- 17 .
Bound With Nasa Tm X-507-18,522-81, Lack No.509-13,515-17,519-21,523-29,531-39,541-46,548-65,567-68,572-80
Author Added Entry:
Spearman,M Leroy;
Copy Details:
Acc. No.: TR14307, Full Call No.: NASA TM X-519, Item type: Technical Report , Location: General Stacks,
------------------------- --------------------- ------ --------- ------- ------- --------- --------