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521. USAAVLABS technical reports. 64-68G. Heavy-lift tip turbojet rotor system: v. 7, Weight and balance studies; prepared by Hiller Aircraft Company, Inc.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Oct. 1965
SuDoc number:: D 117.8/2:(nos.)

522. USAAVLABS technical reports. 64-68H. Heavy-lift tip turbojet rotor system: v. 8, Wind-tunnel studies [with list of references]; prepared by Hiller Aircraft Company, Inc.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Oct. 1965
SuDoc number:: D 117.8/2:(nos.)

523. USAAVLABS technical reports. 64-68J. Heavy-lift tip turbojet rotor system: v. 10, Stability and control [with list of references]; prepared by Hiller Aircraft Company, Inc.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Oct. 1965
SuDoc number:: D 117.8/2:(nos.)

524. USAAVLABS technical reports. 64-68K. Heavy-lift tip turbojet rotor system: v. 11, Engine design.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Oct. 1965
SuDoc number:: D 117.8/2:(nos.)

525. USAAVLABS technical reports. 64-68L. Heavy-lift tip turbojet rotor system: v. 12, Fuel pump and control system design [with list of references].

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Oct. 1965
SuDoc number:: D 117.8/2:(nos.)

526. USAAVLABS technical reports. 64-68M. Heavy-lift tip turbojet rotor system: v. 13, Preliminary model specification for Continental model 357-1 engine.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Oct. 1965
SuDoc number:: D 117.8/2:(nos.)

527. USAAVLABS technical reports. 65-40. Power transmission studies for shaft-driven heavy-lift helicopters [with bibliography]; by Lester R. Burroughs.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Oct. 1965
SuDoc number:: D 117.8/2:(nos.)

528. USAAVLABS technical reports. 65-48. Analytical study of dynamics of aircraft in unsteady flight [with list of refrences; prepared by H. C. Curtiss, jr.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Oct. 1965
SuDoc number:: D 117.8/2:(nos.)

529. USAAVLABS technical reports. 65-52. Main power system for shaft-driven heavy lift helicopters, [with bibliography]; by Robert B. Bossier, jr.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Oct. 1965
SuDoc number:: D 117.8/2:(nos.)

530. USAAVLABS technical reports. 65-56. Transmission study for tandem-rotor shaft-driven heavy-lift helicopters, R-379 [with bibliography]; by J. Mack.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Sept. 1965
SuDoc number:: D 117.8/2:(nos.)

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